Premixed charge compression ignition engine with optimal combustion control

ABSTRACT

A premixed charge compression ignition engine, and a control system, is provided which effectively initiates combustion by compression ignition and maintains stable combustion while achieving extremely low oxides of nitrogen emissions, good overall efficiency and acceptable combustion noise and cylinder pressures. The present engine and control system effectively controls the combustion history, that is, the time at which combustion occurs, the rate of combustion, the duration of combustion and/or the completeness of combustion, by controlling the operation of certain control variables providing temperature control, pressure control, control of the mixture&#39;s autoignition properties and equivalence ratio control. The combustion control system provides active feedback control of the combustion event and includes a sensor, e.g. pressure sensor, for detecting an engine operating condition indicative of the combustion history, e.g. the start of combustion, and generating an associated engine operating condition signal. A processor receives the signal and generates control signals based on the engine operating condition signal for controlling various engine components to control the temperature, pressure, equivalence ratio and\or autoignition properties so as to variably control the combustion history of future combustion events to achieve stable, low emission combustion in each cylinder and combustion balancing between the cylinders.

This application is a continuation of Ser. No. 60/024,515 filed Aug. 23,1996.

TECHNICAL FIELD

This invention relates generally to a compression ignition enginearranged to internally burn a premixed charge of fuel and air usingautoignition to achieve reduced emissions while maintaining the desiredfuel economy.

BACKGROUND OF THE INVENTION

For well over 75 years the internal combustion engine has been mankind'sprimary source of motive power. It would be difficult to overstate itsimportance or the engineering effort expended in seeking its perfection.So mature and well understood are merely designs made up of choicesamong a variety of known alternatives. For example, an improved outputtorque curve can easily be achieved by sacrificing engine fuel economy.Emissions abatement or improved reliability can also be achieved with anincrease in cost. Still other objectives can be achieved such asincreased power and reduced size and/or weight but normally at asacrifice of both fuel efficiency and low cost.

The challenge to contemporary designers has been significantly increasedby the need to respond to governmentally mandated emissions abatementstandards while maintaining or improving fuel efficiency. In view of themature nature of engine design, it is extremely difficult to extractboth improved engine performance and emissions abatement from furtherinnovations of the basic engine designs commercially available today.Yet the need for such innovations has never been greater in view of theseries of escalating emissions standards mandated for the future by theUnited States government and other countries. Attempts to meet thesestandards includes some designers looking for a completely new enginedesign.

Traditionally, there have been two primary forms of reciprocating pistonor rotary internal combustion engines: diesel and spark ignitionengines. While these engine types have similar architecture andmechanical workings, each has distinct operating properties which arevastly different from each other. Diesel and spark ignited engineseffectively control the start of combustion (SOC) using simple, yetdistinct means. The diesel engine controls the SOC by the timing of fuelinjection. In a spark ignited engine, the SOC is controlled by the sparktiming. As a result, there are important differences in the advantagesand disadvantages of diesel and spark-ignited engines. The majoradvantage that a spark-ignited natural gas, or gasoline, engine has overa diesel engine is the ability to achieve extremely low NOx andparticulate emissions levels. The major advantage that diesel engineshave over premixed charge spark ignited engines (such as passenger cargasoline engines and lean burn natural gas engines) is higher thermalefficiency. One key reason for the higher efficiency of diesel enginesis the ability to use higher compression ratios than premixed chargespark ignited engines (the compression ratio in premixed charge sparkignited engines has to be kept relatively low to avoid knock). A secondkey reason for the higher efficiency of diesel engines lies in theability to control the diesel engine's power output without a throttle.This eliminates the throttling losses of premixed charge spark ignitedengines and results in significantly higher efficiency at part load fordiesel engines. Typical diesel engines, however, cannot achieve the verylow NOx and particulate emissions levels which are possible withpremixed charge spark ignited engines. Due to the mixing nature ofdiesel combustion a large fraction of the fuel exists at a very fuelrich equivalence ratio which is known to lead to particulate emissions.Premixed charge spark ignited engines, on the other hand, have nearlyhomogeneous air fuel mixtures which tend to be either lean or close tostoichiometric, resulting in very low particulate emissions. A secondconsideration is that the mixing controlled combustion in diesel enginesoccurs when the fuel and air exist at a near stoichiometric equivalenceratio which leads to high temperatures. The high temperatures, in turn,cause high NOx emissions. Lean burn premixed charge spark ignitedengines, on the other hand, burn their fuel at much leaner equivalenceratios which results in significantly lower temperatures leading to muchlower NOx emissions. Stoichiometric premixed charge spark ignitedengines, on the other hand, have high NOx emissions due to the highflame temperatures resulting from stoichiometric combustion. However,the virtually oxygen free exhaust allows the NOx emissions to be reducedto very low levels with a three-way catalyst.

Relatively recently, some engine designers have directed their effortsto another type of engine which utilizes premixed charge compressionignition (PCCI) or homogeneous charge compression ignition (HCCI),hereinafter collectively referred to as PCCI. Engines operating on PCCIprinciples rely on autoignition of a relatively well premixed fuel/airmixture to initiate combustion. Importantly, the fuel and air are mixed,in the intake port or the cylinder, long before ignition occurs. Theextent of the mixture may be varied depending on the combustioncharacteristics desired. Some engines are designed and/or operated toensure the fuel and air are mixed into a homogeneous, or nearlyhomogeneous, state. Also, an engine may be specifically designed and/oroperated to create a somewhat less homogeneous charge having a smalldegree of stratification. In both instances, the mixture exists in apremixed state well before ignition occurs and is compressed until themixture autoignites. Importantly, PCCI combustion is characterized inthat: 1) the vast majority of the fuel is sufficiently premixed with theair to form a combustible mixture throughout the charge by the time ofignition and throughout combustion; and 2) combustion is initiated bycompression ignition. Unlike a diesel engine, the timing of the fueldelivery, for example the timing of injection, in a PCCI engine does notstrongly affect the timing of ignition. The early delivery of fuel in aPCCI engine results in a premixed charge which is very well mixed, andpreferably nearly homogeneous, thus reducing emissions, unlike thestratified charge combustion of a diesel which generates higheremissions. Preferably, PCCI combustion is characterized in that most ofthe mixture is significantly leaner than stoichiometric toadvantageously reduce emissions, unlike the typical diesel engine cyclein which a large portion, or all, of the mixture exists in a rich stateduring combustion.

An engine operating on PCCI combustion principles has the potential forproviding the excellent fuel economy of the diesel engine whileproviding NOx and particulate emissions levels that are much lower thanthat of current spark-ignited or diesel engine. For example, U.S. Pat.No. 4,768,481 to Wood discloses a process and engine that is intended touse a homogeneous mixture of fuel and air which is spontaneouslyignited. A controlled rate of combustion is said to be obtained byadding exhaust products to the air-fuel mixture. A combustion chamber isconnected to the engine cylinder and fuel gas is supplied to the chambervia a check valve. A glow plug is positioned between the combustionchamber and the cylinder. The mixture entering the combustion is heatedby the glow plug and by the hot walls of the combustion chamber. Themixture ignites due to the increase in temperature and the increase inpressure resulting from compression. The Wood patent is specificallydirected to a two-stroke engine, but generally mentions that thetechnology could be applied to a four-stroke engine. However, thisreference fails to discuss how the exhaust gas recirculation and glowplug would be controlled to optimize the start of combustion and tomaintain the optimal start, and duration, of combustion, as load andambient conditions change. A practical embodiment of this engine isunlikely to be capable of effectively controlling and maintaining PCCIcombustion without additional controls.

U.S. Pat. No. 5,535,716 issued to Soto et al., discloses a compressionignition type engine which greatly reduces NOS emissions by introducingan evaporated fuel/air mixture into the combustion chamber during theintake event and early in the compression event for self-ignitedcombustion later in the compression event. The amount of NOx emissionsproduced by this engine is about one-thirtieth of that produced by adiesel engine. These principles are also set forth in SAE TechnicalPaper No. 960081, Aoyama, T. et al., “An Experimental Study onPremixed-Charge Compression Ignition Gasoline Engine”, Feb. 26, 1996.However, these references do not specifically discuss controlling thetiming of the start of combustion and the rate of combustion. Moreover,the engine disclosed in these references only uses the heat generated bycompression to ignite the charge, without the use of any preheating.Also, these references do not suggest the controls, nor the manner ofoperating the controls, necessary to maintain stable combustion. Also,these references only disclose the use of gasoline.

U.S. Pat. No. 5,467,757 issued to Yanagihara et al., discloses a directinjection compression-ignition type engine in which fuel is injectedinto a combustion chamber during the intake stroke or compressionstroke, before 60 degrees BTDC of the compression stroke, so as toreduce the amount of soot and NOx generated to substantially zero. Theseadvantages are achieved by considerably enlarging the mean particle sizeof the injected fuel from the mean particle size used in conventionalcombustion processes to prevent the early vaporization of injected fuelafter injection and by making the injection timing considerably earlierthan conventional injection timing to ensure a uniformed fusion of theinjected fuel in the combustion chamber. However, this reference nowheresuggests a manner of actively controlling the combustion history, suchas the timing of the start of combustion and/or the duration ofcombustion.

Researchers have used various other names to refer to PCCI combustion.For example, Onishi, et al. (SAE Technical Paper No. 790501, Feb.26-Mar. 2, 1979) called it “ATAC”, which stands for “ActiveThermo-Atmosphere Combustion.” Noguchi, et al. (SAE Technical Paper No.790840, Sep. 10-13, 1979) called it “TS”, which stands for“Toyota-Soken”, and Najt, et al. (SAE Paper No. 830264, 1983) called it“CIHC”, which stands for “compression-ignited homogeneous charge.”

Onishi, et al., worked with two-stroke engines. They found that PCCIcombustion (ATAC) could be made to occur in a two-stroke engine at lowload over a wide speed range. Combustion stability was much better thanin the standard engine and there were significant improvements in fueleconomy and exhaust emissions. Schlieren photography of the combustionwas carried out with results quite similar to those obtained in theircombustion studies. It was found that combustion was initiated at manypoints in the combustion chamber. However, there were small timedifferences between the start of combustion of these many points. Also,the combustion reactions were found to require a relatively long timecompared to conventional spark-ignited flame propagation. To attain PCCIcombustion, the following conditions were found to be important. Thequantity of mixture and the air/fuel ratio supplied to the cylinder mustbe uniform from cycle to cycle. The scavenging “directivity” andvelocity must have cyclic regularity to ensure the correct condition ofthe residual gases remaining in the cylinder. The temperature of thecombustion chamber walls must be suitable. The scavenging passage inletmust be located at the bottom of the crankcase. It was found that atvery light loads, PCCI was not successful because charge temperatureswere too low. At very high loads, PCCI was not successful because theresidual gas quantity was too low. In between these regions, PCCIcombustion was successful.

Noguchi also obtained PCCI combustion in a two-stroke engine. Verystable combustion was observed, with low emissions of hydrocarbons (HC)and improved fuel consumption. Operation in PCCI mode was possiblebetween 800 and 3200 rpm and air/fuel ratios between 11 and 22. Deliveryratios of up to 0.5 could be achieved at idle conditions. They observedthat combustion could start at lower temperatures and pressures thanthose required for conventional diesel combustion. The combustionbehavior was different from that of conventional spark-ignitedcombustion. Ignition occurred at numerous points around the center ofthe combustion chamber and the flame spread rapidly in all directions.The combustion duration was shorter than that of conventionalcombustion. It was proven that ignition kernels were not generated fromcontaminants deposited on the combustion chamber walls (generallypresumed to be the cause of “run-on” phenomena in conventional gasolineengines). To gain a better understanding of the combustion, they set upan experimental apparatus for detecting radicals in the combustionchamber. It was found that the radicals showed higher peaks of luminousintensity that disappeared at an earlier time than with conventionalspark-ignited combustion. In the case of conventional spark-ignitioncombustion, all the radicals such as OH, CH, C₂, H, and CHO, HO₂, O wereobserved at almost the same crank angle. However, with PCCI combustion,CHO, HO₂ and O radicals were detected first, followed by HC, C₂, and Hradicals, and finally the OH radical.

Najt, et al. were able to achieve PCCI combustion in a four-strokeengine. They used a CFR single-cylinder engine with a shrouded intakevalve. Several compression ratios were tried, and it was found that,although higher ratios would allow combustion at lower charge gastemperatures, they also resulted in excessively fast heat release rates.While a compression ratio of 7.5:1 was satisfactory, a compression ratioof 10:1 was not. Intake temperatures were in the range of 480° K. to800° K. Their average energy release rates were considerably higher thanthose measured by Onishi and Noguchi.

SAE Paper No. 960742, entitled “Improving the Exhaust Emissions ofTwo-Stroke Engines by Applying the Activated Radical Combustion”,Ishibashi, Y. et al., 1996, is noted as disclosing yet another study ofPCCI combustion in a two-stroke engine.

Although Onishi et al., Noguchi et al., Naijt et al. and Ishibashi, etal. have made significant progress in understanding PCCI combustion,these references fail to suggest a practical PCCI engine having acontrol system capable of maintaining stable, efficient PCCI combustionwith low emissions by controlling the time at which combustion occurs,the duration of combustion, the rate of combustion and/or thecompleteness of combustion. Specifically, these references do notsuggest a PCCI engine and control system capable of effectivelycontrolling the start of combustion. Moreover, these references do notsuggest a system capable of actively enhancing the engine startabilityand achieving combustion balancing between the cylinders in amulti-cylinder engine.

SAE Technical Paper No. 892068, entitled “Homogeneous-Charge CompressionIgnition (HCCI) Engines”, Thring, R., Sept. 15, 1989, investigated PCCIoperation of a four stroke engine. The paper found that PCCI requiredhigh exhaust gas recirculation (EGR) rates and high intake temperatures.It was shown that PCCI combustion produces fuel economy resultscomparable to a direct injection diesel engine and, that under favorableconditions, i.e. equivalence ratio of 0.5 and EGR rate of 23%, producesvery low cyclic irregularity. This study also concluded that before PCCIcan be made practical, it will be necessary to operate an engine in thePCCI mode without the need to supply large amounts of heat energy to theintake. The paper suggests two possibilities: the use of heated surfacesin the combustion chamber and the use of multi-stage turbochargingwithout intercoolers. However, although this paper suggests furtherinvestigating the effects of EGR and intake temperature on the timing ofthe start of combustion, this paper fails to disclose a system foreffectively achieving active control of the start and duration ofcombustion.

U.S. Pat. No. 5,476,072 to inventor discloses another example of a PCCIengine which includes a cylinder head design that prevents excessivestresses and structural damage that PCCI engines inherently tend tocause. Specifically, the head includes a movable accumulator pistonwhich moves to limit the peak cylinder pressure and temperature;however, control over the movement of the piston is merely passive and,therefore, this engine is unlikely to effectively stabilize combustion.Moreover, this reference nowhere suggests controlling the timing atwhich rapid combustion occurs, nor how such control could beaccomplished.

An October 1951 publication entitled “Operating directions—LOHMANNBICYCLE MOTOR” discloses a two-stroke engine operating on PCCIcombustion principles. Compression ratio is continuously adjustablebased on outside temperature, fuel, speed and load. However, this enginerequires the operator control the compression ratio manually. Therefore,this engine could not provide effective active control of combustion toensure efficient combustion with low emissions throughout all operatingconditions. Also, manual adjustment of compression ratio alone, withoutautomatic temperature, equivalence ratio and\or autoignition propertycontrol, will not result in stable, optimized combustion throughout alloperating conditions.

Conventional “dual fuel” engines operate on both a gaseous fuel mixtureand diesel fuel. However, conventional dual fuel engines utilize thetiming of the injection of diesel fuel to control the SOC of thefuel/air mixture received from the intake duct. In order to achieve thisresult, dual fuel engines inject the diesel fuel at approximately topdead center. In addition, the quantity of diesel fuel injected in a dualfuel engine is sufficient to ensure that the gaseous fuel in thecombustion chamber ignites and burns virtually completely. As a result,dual fuel engines produce emissions similar to most conventional dieseland natural gas engines. In particular, in known dual fuel engines usingdiesel fuel and natural gas at high load, only a small amount of dieselfuel is required to start ignition and the emissions produced would besimilar to a spark ignited natural gas engine. Under other conditionswhen substantial diesel fuel is injected, the emissions produced wouldbe similar to a conventional diesel engine.

Consequently, there is a need for an engine operating on PCCI principleswhich includes a combustion control system capable of effectivelycontrolling the timing of the start of combustion or location ofcombustion, and the rate or duration of combustion during engineoperation.

SUMMARY OF THE INVENTION

A general objective of the subject invention is to overcome thedeficiencies of the prior art by providing a practical PCCI engine and acontrol system for effectively and efficiently operating the PCCIengine.

Another object of the present invention is to provide a PCCI engine andcontrol scheme for controlling the engine in a manner to optimallyminimize emissions, especially oxides of nitrogen and particulateemissions, while maximizing efficiency.

Yet another object of the present invention is to provide a PCCI engineand control system for optimally controlling the combustion history ofsubsequent combustion events to effectively control the combustionevent.

Still another object of the present invention is to provide a PCCIengine and control system for effectively controlling PCCI combustion insuch a manner to achieve acceptable cylinder pressure while minimizingcombustion noise.

A further object of the present invention is to provide a PCCI engineand control system which operates to actively control the combustionhistory of future combustion events during engine operation by sensingan engine operating condition indicative of the combustion history.

A still further object of the present invention is to provide a PCCIengine and control system which effectively controls various engineoperating control variables to control the time at which the combustionevent occurs during the compression and expansion events of the engine.

Yet another object of the present invention is to provide a PCCI engineand control system which effectively ensures that combustion occurs atan appropriate crank angle during the engine cycle to ensure stablecombustion, low emissions, acceptable pressure levels and optimumefficiency.

Another object of the present invention is to provide a PCCI engine andcontrol system which effectively controls the temperature, pressure,equivalence ratio and/or air/fuel mixture autoignition properties toprecisely control the timing of the start of combustion.

A still further object of the present invention is to provide a PCCIengine and control system which effectively achieves continuous, stablePCCI combustion while achieving acceptable cylinder pressures and thedesired brake mean effective pressure.

Yet another object of the present invention is to provide a PCCI engineand control system which effectively controls the commencement ofcombustion and the combustion rate so as to ensure that substantiallyall of the combustion process occurs within an optimal crank anglelimit, i.e. 20 degrees through 35 degrees ATDC, while minimizingemissions and maximizing efficiency.

Another object of the present invention is to provide a PCCI enginewhich can be easily started.

Still another object of the present invention is to provide amulti-cylinder PCCI engine and control system which effectivelyminimizes variations in the combustion events of the cylinders.

Yet another object of the present invention is to provide amulti-cylinder PCCI engine and control system which effectively controlsthe start of combustion to achieve stable, low emission, efficientcombustion throughout exposure to changes in engine load and ambientconditions.

Another object of the present invention is to provide a control systemfor a PCCI engine which effectively detects or senses the start ofcombustion to provide feedback control and then controls the operatingconditions of the engine to optimize the start of combustion.

Still another object of the present invention is to provide a PCCIengine and control system which effectively minimizes the unburnedhydrocarbon and carbon monoxide emissions.

The above objects and others are achieved by providing a premixed chargecompression ignition internal combustion engine, comprising an enginebody, a combustion chamber formed in the engine body and combustionhistory control system for controlling a combustion history of futurecombustion events to reduce emissions and optimize efficiency. Thecombustion history control system includes at least one of a temperaturecontrol system for varying the temperature of the mixture of fuel andair, a pressure control system for varying the pressure of the mixture,an equivalence ratio control system for varying an equivalence ratio ofthe mixture and a mixture autoignition property control system forvarying an autoignition property of the mixture. The engine furtherincludes an operating condition detecting device for detecting an engineoperating condition indicative of the combustion history and generatingan engine operating condition signal indicative of the engine operatingcondition, and a processor for receiving the engine operating conditionsignal, determining a combustion history value based on the engineoperating condition signal, and generating one or more control signalsbased on the combustion history value. The one or more control signalsare used to control at least one of the temperature control system, thepressure control system, the equivalence ratio control system and themixture autoignition property control system to variably control thecombustion history of future combustion events.

The engine operating condition detecting device may include a start ofcombustion sensor for sensing the start of combustion and generating astart of combustion signal. Also, the combustion history value may bedetermined based on the start of combustion signal. The engine operatingcondition detecting device may be a cylinder pressure sensor.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1a is a schematic diagram of one embodiment of the presentinvention showing a single cylinder of the engine of FIG. 1b andassociated control system;

FIG. 1b is a schematic diagram of a multi-cylinder engine of the presentinvention;

FIG. 2 is a graph showing cylinder pressure and heat release rate as afunction of crank angle for the PCCI engine of the present invention;

FIG. 3 is a graph showing the apparent heat release rate as a functionof crank angle for several different engine operating conditions;

FIG. 4a is a graph showing knock intensity as a function of time for agiven set of operating conditions;

FIG. 4b is a graph showing gross indicated mean effective pressure(GIMEP) as a function of time;

FIG. 4c is a graph showing peak pressure as a function of time for thesame conditions of FIGS. 4a and 4 b;

FIG. 5 is a graph showing apparent heat release rate as a function ofcrank angle and illustrating the increase in the heat release rateduration as the combustion or heat release location or timing isretarded;

FIG. 6 is a graph showing cylinder pressure as a function of crank angleand illustrating the decrease in peak cylinder pressure as the heatrelease rate retards;

FIG. 7a. is a graph showing GIMEP as a function of intake manifoldtemperature for two different engine speed cases;

FIG. 7b is a graph showing the coefficient of variation of GIMEP as afunction of intake manifold temperature for two different engine speedcases;

FIG. 7c is a graph showing peak cylinder pressure as a function ofintake manifold temperature for two different engine speeds;

FIG. 7d is a graph showing the start of combustion as a function ofintake manifold temperature for two different engine speeds;

FIG. 7e is a graph showing heat release duration in crank angle degreesas a function of intake manifold temperature for two different enginespeeds;

FIG. 7f is a graph showing heat release duration in time as a functionof intake manifold temperature for two different engine speeds;

FIG. 7g is a graph showing gross indicated thermal efficiency as afunction of intake manifold temperature for two different engine speeds;

FIG. 7h is a graph showing fuel specific hydrocarbons as a function ofintake manifold temperature for two different engine speeds;

FIG. 7i is a graph showing fuel specific carbon monoxide as a functionof intake manifold temperature for two different engine speeds;

FIG. 7j is a graph showing fuel specific oxides of nitrogen emissions asa function of intake manifold temperature for two different enginespeeds;

FIG. 7k is a graph showing noise as a function of intake manifoldtemperature for two different engine speeds;

FIG. 8 is a graph showing apparent heat release rate as a function ofcrank angle for three different intake manifold temperatures;

FIG. 9 is a graph showing both the start of combustion and combustionduration as a function of wall temperature;

FIG. 10 is a graph showing both the start and end of combustion as afunction of crank angle for a given time period, and GIMEP for the sametime period, wherein a glow plug is cycled;

FIG. 11 is a graph showing the apparent heat release rate as a functionof crank angle for the glow plug transient of FIG. 10;

FIG. 12 discloses one embodiment of an end cylinder compensating systemof the present invention for providing cylinder-to-cylinder temperaturecontrol;

FIG. 13 is a schematic diagram of a second embodiment of the endcylinder compensating device for providing cylinder-to-cylindertemperature control;

FIG. 14 is a graph showing the effects of changing intake and exhaustvalve opening and closing events on top dead center (TDC) temperature;

FIG. 15 is a graph showing the effects of changing intake and exhaustvalve opening and closing events, and variable compression ratio, on theresidual mass fraction and temperature at top dead center;

FIG. 16 is a graph showing both cylinder pressure and heat release as afunction of crank angle for different exhaust valve lash settings;

FIG. 17 is a graph showing the effects of varying exhaust gasrecirculation (EGR) on the location of the heat release rate relative tothe crank angle and the effect of variations in EGR on the magnitude ofthe heat release rate;

FIG. 18 is a graph showing the effect of varying the EGR rate on thetiming of the start of combustion;

FIG. 19 is a schematic of an improved engine of the present inventionhaving one cylinder operating under PCCI conditions to optimize the useof EGR;

FIG. 20 is a graph showing the effects of changing compression ratio onthe temperature at top dead center;

FIG. 21 is a graph showing the start of combustion as a function ofintake manifold temperature and the effects of changing the compressionratio on the start of combustion and intake manifold temperature;

FIG. 22a is a partial cross sectional view of one cylinder of the PCCIengine of the present invention including one embodiment of acompression ratio varying device;

FIG. 22b is a partial cross sectional view of one cylinder of the PCCIengine of the present invention showing a second embodiment of acompression ratio varying device;

FIG. 22c is a partial cross sectional view of one cylinder of thepresent PCCI engine showing a third embodiment of the compression ratiovarying device;

FIG. 22d is a partial cross sectional view of a single cylinder of thepresent PCCI engine showing a fourth embodiment of the compression ratiovarying device of the present invention;

FIG. 23 is a schematic diagram of an opposed piston PCCI engine of thepresent invention including a variable phase shifting mechanism forvarying the compression ratio;

FIG. 24 is a side view of the differential mechanism used in thevariable phase shifting mechanism of FIG. 23;

FIG. 25 is a graph showing compression ratio as a function of thedegrees out of phase of two pistons in the opposed piston engine, forexample, of FIG. 23 illustrating various compression ratio settings;

FIG. 26 is a graph showing cylinder volume as a function of crank angleof a reference piston in an opposed piston PCCI engine which shows thatthe compression ratio decreases as the pistons become more out of phase;

FIG. 27 is a graph showing the effects of changing intake and exhaustvalve opening and closing events, and varying the compression ratio, onthe percent of baseline airflow rate and the TDC temperature;

FIG. 28 is a graph showing the effects of changes and intake in exhaustvalve opening and closing events, and varying the compression ratio, onthe diesel equivalent brake specific fuel consumption and TDCtemperature;

FIG. 29 is a graph showing the effects of changes and intake in exhaustvalve opening and closing events, and variations in compression ratio,on peak cylinder pressure and TDC temperature;

FIG. 30 is a graph showing the effects of water injection on intakemanifold temperature and temperature at top dead center;

FIG. 31a is a graph showing the combustion duration in crank angledegrees as a function of intake manifold pressure (IMP);

FIG. 31b is a graph showing combustion duration in time as a function ofIMP;

FIG. 31c is a graph showing the effect of changes in IMP on themagnitude and timing or location of the heat release rate;

FIG. 31d is a graph showing the start of combustion timing and crankangle degrees as a function of IMP;

FIG. 31e is a graph showing fuel specific hydrocarbons as a function ofIMP;

FIG. 31f is a graph showing GIMEP as a function of IMP;

FIG. 31g is a graph showing gross indicated thermal efficiency as afunction of IMP;

FIG. 31h is a graph showing fuel specific carbon monoxide as a functionof IMP;

FIG. 31i is a graph showing fuel specific oxides of nitrogen emissionsas a function of IMP;

FIG. 31j is a graph showing the coefficient of variation of GIMEP as afunction of IMP;

FIG. 31k is a graph showing the peak cylinder pressure as a function ofIMP;

FIG. 31l is a graph showing noise as a function of IMP;

FIG. 31m is a graph showing the effects of increasing IMP on peakcylinder pressure and GIMEP;

FIG. 32 is a graph showing the effect of various trace species on astart of combustion and temperature;

FIG. 33 is a graph showing the effects of additional amounts of ozone onadvancing the start of combustion;

FIG. 34 is a graph showing the effect of varying the type of fuel usedin the present PCCI engine on the start of combustion wherein theincrease in temperature indicates the start of combustion;

FIG. 35 is a graph showing the apparent heat release duration as afunction of equivalence ratio;

FIG. 36 is a graph showing the start of combustion in crank angledegrees as a function of equivalence ratio;

FIGS. 37 is a graph showing the effects of variations in equivalenceratio on the start of combustion wherein an increase in temperatureindicates the start of combustion;

FIG. 38 is a graph showing the effects of variations in the equivalenceratio on the magnitude and timing, or location, of the heat releaserate;

FIG. 39 is a graph showing the effects of equivalence ratio on thecompressor pressure ratio and the compressor outlet temperature;

FIG. 40 is a graph showing the effects of varying the equivalence ratioon the brake specific fuel consumption;

FIG. 41 is a graph showing the differences in pumping mean effectivepressure and GIMEP for two differently sized turbine casings;

FIG. 42 is a graph showing the diesel equivalent BSFC and BMEP for twodifferently sized turbine casings;

FIG. 43 is a graph showing the turbine rotor speed and intake manifoldpressure for two differently sized turbine casings;

FIG. 44 is a graph showing the fuel specific oxides of nitrogenemissions for PCCI combustion with various fuels in comparison to atypical compression ignition diesel engine;

FIG. 45 is a graph showing emissions as a function of engine speed;

FIG. 46 is a graph showing emissions as a function of temperature atbottom dead center;

FIG. 47 is a graph showing fuel specific carbon monoxide as a functionof end of combustion flame temperature;

FIGS. 48a-50 b are partial cross sectional views of a single cylinder ofthe PCCI engine of the present invention showing an alternativeembodiment including various crevice minimizing features; and

FIG. 51 is a graph showing the effects of various percentages of dieselpilot injections on the heat release rate location and shape.

DETAILED DESCRIPTION OF THE INVENTION

The present invention is directed to an improved premixed chargecompression ignition (PCCI) engine and control scheme for controllingthe engine in a manner to optimally minimize emissions while maximizingefficiency. For the purposes of this application, PCCI refers to anyengine or combustion process in which: 1) the vast majority of the fuelis sufficiently premixed with the air to form a combustible mixturethroughout the charge by the time of ignition and throughout combustion;and 2) combustion is initiated by compression ignition. PCCI also refersto any compression ignition engine or combustion process in which thefuel and air are premixed long before ignition. As a result, the timingof injection of the fuel in the PCCI engine does not affect the timingof ignition of the fuel/air mixture. Also, it should be understood thatPCCI is meant to encompass homogeneous charge compression ignition(HCCI) engines and processes wherein the mixture exists in ahomogeneous, or nearly homogeneous state, at the start of combustion. Inthe present invention, the fuel/air mixture is thoroughly mixed to forma very lean homogeneous mixture, or is mixed in a manner to form a lesshomogeneous mixture with a desired air/fuel stratification, to ensurerelatively even, low flame temperatures which result in extremely lowoxides of nitrogen (NOx) emissions. It should be understood the someengines operate under PCCI conditions continuously while other enginesmay operate under PCCI conditions for only a limited period of operationeither by design or inadvertently.

Applicants have recognized that the key to producing a commerciallyviable PCCI engine lies in the control of the combustion history ofsubsequent or future combustion events in such a manner so as to resultin extremely low NOx emissions combined with very good overallefficiency, combustion noise control and with acceptable cylinderpressure. The combustion history may include the time at whichcombustion occurs (combustion timing), the rate of combustion (heatrelease rate), the duration of combustion and/or the completeness ofcombustion. Applicants have determined that the combustion history, andespecially the combustion timing, is sensitive to, and varies dependingon, a variety of factors including changes in load and ambientconditions. The engine and control system of the present inventionoperates to actively control the combustion history of future combustionevents during engine operation to ensure the desired combustion andengine operation is maintained. In the preferred embodiment, the presentengine and control system controls the combustion timing during thecompression and expansion events of the engine.

FIGS. 1a and 1 b illustrates the PCCI engine and control system of thepresent invention, indicated generally at 10. FIG. 1a shows a singleengine cylinder 12 of the multi-cylinder reciprocating piston typeengine shown in FIG. 1b . Of course, the PCCI control system of thepresent invention could be used to control PCCI combustion in an enginehaving only a single cylinder or any number of cylinders, for example, afour, six, eight or twelve cylinder internal combustion engine. Inaddition, although the present PCCI control system is primarilydiscussed with reference to a four stroke engine, the present controlsystem could be applied to a two stroke engine. Also, the PCCI system ofthe present invention may be adapted for use on any internal combustionengine having compression, combustion and expansion events, including arotary engine and a free piston engine.

As shown in FIG. 1a, a piston 14 is reciprocally mounted in the cylinderto form a combustion chamber 13. The piston transmits forces generatedby a combustion event into a conventional engine drive system. Referringto FIGS. 1a and 1 b, an intake air system 23 including an intakemanifold supplies intake air, or an air/fuel mixture to a respectiveintake port 26 associated with each cylinder 12. Likewise, an exhaustgas system 27 including an exhaust manifold 17 receives exhaust gasesflowing from exhaust ports 31. One or more intake valves, such an intakevalve 19 and one or more exhaust valves, such as exhaust valve 21, aremoved between open and closed positions by a conventional valve controlsystem, or a variable valve timing system, to control the flow of intakeair or air/fuel mixture into, and exhaust gases out of, the cylinder,respectively.

The PCCI system 10 includes a combustion sensor 16 for sensing ordetecting an engine operating condition indicative of the combustionhistory and generating a corresponding signal 18. In the preferredembodiment, sensor 16 permits effective combustion control capability bydetecting an engine operating condition or parameter directly relatedto, or indicative of, the time at which the combustion event occursduring the compression and/\or expansion strokes, i.e. preferably thestart of combustion (SOC). For example, a cylinder pressure sensor maybe provided on any or all engine cylinders for sensing, on acycle-by-cycle basis, the SOC. In this case, the sensor 16 also providesother engine condition data, such as the combustion rate, combustionduration, combustion event or heat release location and end ofcombustion data, any one of which may be used instead of the start ofcombustion data. Any conventional means for detecting the start ofcombustion may be used, for example, by sensing the very rapid increasein the cylinder pressure. Other forms of sensors could be used includingaccelerometers, ion probes, optical diagnostics, strain gages and/orfast thermocouples in the cylinder head, liner or piston. Also, torqueor RPM sensors could be used to detect changes in engine torque and RPMassociated with each combustion event. Alternatively, or additionally,an emissions sensor could be used to detect emissions having a knowncorrelation to the completeness of combustion.

Sensor 16 provides feedback control to an electronic control unit 20(ECU). ECU 20 receives signal 18, processes the signal and determines anactual combustion history value, i.e. start of combustion value. Theactual combustion history value is then compared to a predetermineddesired combustion history value obtained, for example, from a look-uptable. Based on the comparison of the actual combustion history value tothe desired combustion history value, ECU 20 then generates a pluralityof output signals, indicated at 22, for variably controlling respectivecomponents of the system so as to effectively ensure, in the preferredembodiment, that the SOC and completion of combustion occur between 20degrees before top dead center (BTDC) during the compression stroke and35 degrees after top dead center (ATDC) during the power stroke of thepiston thereby minimizing NOx emissions while maximizing engineefficiency. The PCCI combustion control scheme is most preferablyimplemented in software contained in ECU 20 that includes a centralprocessing unit such as a micro-controller, micro-processor, or othersuitable micro-computing unit.

As discussed herein, PCCI system 10 may include various components foroptimizing the combustion event. The objectives of the present system,i.e. low oxides of nitrogen (NOx) emissions, high efficiency, etc, maybe achieved using any one of the various control components, or anycombination of the components. In particular, as shown in FIG. 1b, acompressor 24 may be provided along an intake air system 23 upstream ofintake manifold 15 for varying the boost intake pressure. Compressor 24may be driven by any conventional means, such as an exhaust gas driventurbine 25. A bypass circuit 33 including a waste gate valve 43 may beprovided in a conventional manner. A second compressor or supercharger58 may be provided upstream of compressor 24. Supercharger 58 ismechanically driven by the engine drive system. A charge air cooler 28may also be provided downstream of compressor 24. Also, an intake airheater 30 (such as a burner, heat exchanger or an electric heater) maybe provided, for example, after cooler 28 as shown in FIG. 1b, oralternatively, upstream of compressor 24. Also, an individual heater 29may be provided in the intake port 26 associated with each cylinder 12to provide quicker control of the intake manifold temperature for eachcylinder to enhance both individual cylinder combustion control andbalancing of combustion between the cylinders. Compressor 24, cooler 28and heater 30 each include control devices for varying the effect of theparticular component on the pressure/temperature of the intake air ormixture. For example, a bypass valve or waste gate 43 could be used toregulate the amount of exhaust gas supplied from the associated exhaustsystem, which is connected to an exhaust duct 31, to turbine 25 therebyvarying the intake pressure as desired. Similarly, a control valve couldbe provided in the cooling fluid flow path supplied to cooler 28 topermit variable control of the cooling effect of cooler 28. Likewise,various types of variable controls could be used to vary the heatingeffect of heater 30. Output signals 22 from ECU 20 are supplied to thevarious control devices to control compressor 24, cooler 28 and heater30 so as to variably control the pressure preferably and temperature ofthe intake air or mixture on a cycle-by-cycle basis.

In addition, the PCCI system 10 may include a plurality of fuel supplies32 and 34 for supplying fuels having different autoignition properties(for example, different octane or methane ratings, or activation energylevels) into the intake air flow. Fuel control valves 39 and 41 are usedto control the amount of each fuel supply 32, 34 delivered,respectively. For example, fuel may be supplied along the intake airpath between cooler 28 and air heater 30 as shown in FIG. 1b. Of course,fuel could be introduced at various locations along the intake of theengine, such as upstream of the cooler, e.g. upstream of the compressor.Alternatively, the fuel could be injected, by for example an injector35, into the respective intake duct 26 associated with each cylinder, asshown in FIG. 1a.

The present PCCI system 10 also importantly includes a variablecompression ratio means 38 for varying the compression ratio so as toadvantageously advance or retard the combustion event as desired. Forexample, variable compression ratio means 38 may be in the form of acontrol mechanism for varying the shape of the combustion chamber orheight of the piston to vary the effective compression ratio. Theeffective compression ratio could also be varied by varying the timingof closing of intake valve 19 as discussed more fully hereinbelow. Thevariations in the timing of opening and closing of the intake andexhaust valves may be accomplished using any conventional variable valvetiming actuator system capable of receiving signals from ECU 20 andeffectively varying the opening and/or closing of the valves inaccordance with the principles set forth hereinbelow.

In addition, in-cylinder diluent injection may be accomplished using aninjector 40 for injecting a gas or liquid, e.g. air, nitrogen, carbondioxide, exhaust gas, water, etc., into the cylinder to vary thetemperature and the temperature distribution in the cylinder so as tocontrol the combustion event. Similarly, a diluent may be injected intointake duct 26 using, for example, an injector 42.

The present PCCI system may also include a fuel injector 36 forinjecting fuel 37, e.g. diesel fuel, directly into the combustionchamber. Fuel 37 would be injected either early in the compressionevent, preferably approximately between 180 degrees and 60 degrees BTDC,as described below, or later in the compression event near TDC.

By injecting the fuel 37 early in the compression event, it is much morethoroughly mixed with the fuel/air mixture received from the intake ductthan would be the case for a diesel engine, thus ensuring a moredesirable combustion process, in particular the fuel will burn at aleaner equivalence ratio which results in much lower NOx emissions. Thestart or initiation of the combustion (SOC) of the fuel/air mixturereceived from the intake duct may be varied by controlling the quantityof fuel 37 injected. For instance, an earlier combustion event may beachieved by increasing the quantity of fuel 37 while the timing of thecombustion event may be delayed by decreasing the quantity of fuel 37injected.

By injecting the fuel 37 later in the compression stroke, that is nearTDC, conventional diesel fuel injection systems can be used. Thisapproach could be combined with the introduction of one or moreadditional types of fuel in the intake manifold to achieve a PCCI modeof operation. In particular, the fuel injected into the intake manifoldwould have a higher excess air ratio. The excess air ratio is the actualair-fuel ratio of the engine divided by the air-fuel ratio atstoichiometric conditions. For the very lean excess air ratio,combustion along a flame front is impossible. However, autoignition ispossible thereby allowing combustion of a mixture that would be too leanto burn in a typical spark-ignited engine. Applicants have determinedthat PCCI combustion does not initiate at, and propagate out from, asingle location. On the contrary, the results show that combustionincludes multiple ignition sites distributed throughout the combustionchamber.

For efficient, low emission PCCI combustion, it is important to havecombustion occur during an appropriate crank angle range during theengine cycle. If combustion starts too early, cylinder pressures will beexcessively high and efficiency will suffer. If combustion starts toolate, then combustion will be incomplete resulting in poor HC emissions,poor efficiency, high carbon monoxide (CO) emissions, and poorstability. Applicants have determined that the timing of the SOC and thecombustion rate, and therefore combustion duration, in a PCCI engineprimarily depend on the temperature history; the pressure history; fuelautoignition properties, e.g. octane/methane rating or activationenergy, and trapped cylinder charge air composition (oxygen content,EGR, humidity, equivalence ratio etc.). The present invention presents astructured approach to affecting these variables in such a way that thestart of combustion and/or the combustion rate (heat release rate) canbe controlled through various combinations of features discussed morefully hereinbelow.

The various control features for controlling the start of combustion andthe combustion rate are controlled/varied to ensure optimum combustionthroughout engine operating conditions so as to achieve low NOxemissions and high efficiency. Application of these control featureswill cause combustion to occur within a preferred crank angle rangerelative to the top dead center position of the engine piston.Specifically, applicants have recognized that substantially all of thecombustion event should occur between 20 crank angle degrees BTDC and 35crank angle degrees ATDC. Also, combustion would be initiated,preferably between 20 crank angle degrees BTDC and 10 crank angledegrees ATDC, and ideally, approximately between 10 degrees BTDC and 5degrees ATDC. In addition, the duration of the combustion event willtypically correspond to a crank angle in the range of 5-30 crank angledegrees. Preferably, however, one or more of the control features listedbelow will be controlled to prolong the duration of combustion toapproximately 30-40 degrees to achieve desirable peak cylinder pressuresand reduced noise. Thus, optimal control of one or more of the followingfeatures will effectively control the start of combustion and/or therate of combustion such that substantially all of the combustion eventoccurs between 20 crank angle degrees BTDC and 35 crank angle degreesATDC. Of course, there may be conditions under which the start ofcombustion occurs outside the above-stated crank angle range and/or theduration of combustion in the PCCI engine occurs over a broader crankangle range, or may extend beyond the limit described above.

Applicants have shown that stable, efficient PCCI combustion can beachieved with most of the heat release occurring after TDC. For example,as shown in FIG. 2, the centroid of heat release may be positioned at 5°ATDC. Applicant have determined that, at light load and lean conditions,as shown in FIG. 3, heat release duration may be in the range ofapproximately 21.5-25 crank angle degrees.

As shown in FIGS. 4a, 4 b and 4 c, applicants have determined that withan engine running close to its misfire limit, the SOC and end ofcombustion (EOC) progressively retard and heat release durationlengthens. Gross indicated mean effective pressure (GIMEP) passesthrough a maximum as the SOC retards to after TDC. Meanwhile, the knockintensity and peak cylinder pressure (PCP) decrease substantially closeto the misfire limit, while GIMEP remains acceptable. As shown in FIG.5, the peak heat release rate also decreases and the heat releaseduration increases as the misfire limit is approached. Meanwhile, asshown in FIG. 6, the peak cylinder pressure decreases as the heatrelease rate retards. Clearly, the engine cannot sustain this reactionprocess without providing the appropriate controls discussed herein.Applicants have determined that the best operating point occurs with theSOC occurring a few degrees after TDC. Certainly, improving thePCP-GIMEP tradeoff for PCCI combustion requires a SOC after TDC. As aresult, it is clear that variable, active control is necessary tomaintain the SOC and duration of combustion at the desired location andat the desired length, respectively, to achieve effective, efficientPCCI combustion.

Variation in the SOC, between sequential combustion events in a singlecylinder engine and between cylinders in a multi-cylinder engine, is dueto the sensitivity of PCCI combustion to the pressure and temperaturehistory leading up to the particular combustion event. Very smallvariations in the compression ratio, the amount of trapped residual,wall temperatures, etc. have a significant effect on the pressure andtemperature history. The present PCCI engine and method of operating theengine include control variables/features capable of compensating for,and controlling, these variations to achieve optimum PCCI combustion.

Generally, the control variables, which can be used to effectivelycontrol the commencement of combustion and the combustion rate so as toensure that substantially all of the combustion process occurs withinthe optimal crank angle limit, i.e. 20 degrees BTDC through 35 degreesATDC while minimizing emissions and maximizing efficiency, may beclassified in four categories of control: temperature control; pressurecontrol; control of the mixture's autoignition characteristic; andequivalence ratio control.

Temperature Control

The temperature of the in-cylinder air/fuel mixture (in-cylindertemperature) plays an important role in determining the start ofcombustion. The in-cylinder temperature may be varied to control thestart of combustion by varying certain key control features, such ascompression ratio (CR), intake manifold temperature (IMT), exhaust gasrecirculation (EGR), residual mass fraction (RMF), heat transfer andtemperature stratification.

Applicants have determined that intake manifold temperature (IMT) has asignificant effect on propane-fueled PCCI combustion. During two ofApplicants' studies, engine speed, equivalence ratio (0) and intakemanifold pressure (IMP) were held constant while IMT was swept throughthe practical operating range. The lowest IMT was limited by unstableoperation and the highest IMT was limited by maximum allowable peakcylinder pressure (PCP). The conditions of the first and second studies,respectively, included engine speed=1200 rpm and 2000 rpm; equivalenceratio=0.30 and 0.24; and IMP=3.3 bar and 4.1 bar. As shown in FIGS. 7aand 7 b, increasing IMT resulted in increased GIMEP and a decreasedcoefficient of variation (CoV) of GIMEP. Also, increasing IMT increasedthe PCP as shown in FIG. 7c, while advancing the SOC and decreasingcombustion duration (FIGS. 7d-7 f). Increasing IMT also increased grossindicated thermal efficiency (FIG. 7g) and the estimated noise (FIG.7k). With respect to emissions, increasing IMT decreased FSHC emissions(FIG. 7h), decreased fuel specific carbon monoxide (FSCO) emissions(FIG. 7i), but had no observable effect on FSNOx (FIG. 7j).

In summary, Applicants have determined that small changes in IMT havelarge effects on many aspects of propane-fueled PCCI combustion. Byvarying the intake temperature, the combustion event can be advanced orretarded. Increasing the intake temperature will advance the start ofcombustion; decreasing the intake temperature will retard the start ofcombustion, as shown graphically in FIG. 8. This temperature control maybe accomplished using heat exchangers or burners. For example, a chargeair cooler may be positioned along the intake manifold. A burner orheater in combination with a cooler offers exceptional intaketemperature control. The exhaust products of the burner may be directlymixed with the intake air, the burner could use the intake air directlyfor its air supply, or the heat generated by the burner could be addedto the intake air through a heat exchanger. The heat exchanger may usewaste heat in engine coolant or exhaust gases to heat the intake air.Also, rapid control of IMT can be achieved by using a charge air coolerbypass. A regenerator (similar to that used in a Stirling engine) couldbe used to recover and transfer exhaust heat into the intake air througha heat exchanger thereby controlling the intake temperature. Inaddition, IMT could be varied by injecting fuel into the manifold indifferent phases, e.g. as a liquid or a gas. The change in the heatrequired for vaporization of a liquid fuel would reduce IMT. Of course,different types of fuels would have different effects on IMT.

Applicants have also determined how residual and intake temperature,boost and combustion chamber and port wall heat transfer, affectin-cylinder bulk temperature throughout intake and compression, and alsothe effect on spatial temperature distribution at TDC. Specifically,Applicants compared the intake and compression events for an enginerunning on an air and propane mixture. Applicants determined that thetemperature at the SOC is also determined in part by the reheating ofthe intake charge by existing heat energy. For the purposes of thisapplication, reheat is defined as T(average in-cylinder @ intake valveclosing (IVC))—T(average intake manifold), that is, the differencebetween intake manifold temperature, i.e. temperature assigned at theinlet to the port and the in-cylinder bulk temperature at IVC.Applicants determined that reheat starts in the port and continuesin-cylinder. Moreover, 56% of reheat was due to wall heat transfer and44% due to mixing and boost for the condition examined. Clearly, heattransfer is very important in determining reheat.

One study that elucidates the importance of the wall temperatures on thein-cylinder heat transfer is the following. In comparing the firingcylinder to the misfiring cylinder, it was noted that the misfiringcylinder's reheat was 63% of the firing case (27 vs 43 K). Lower walltemperatures for a misfiring cylinder compared to a firing cylinder arethe main reason for its lower in-cylinder temperatures. The firingcylinder had a TDC in-cylinder temperature 46 K higher than a misfiringcylinder, compared to a 16 K higher temperature at IVC. If compressionwere done adiabatically for each case, the temperature difference at TDCwould have been ˜35 K given the initial 16 K difference. Therefore, ˜11K (46-35 K) temperature loss from IVC to TDC is due to cooler misfiringwall temperatures. Interestingly, although walls heat the in-cylindergases for the majority of the intake and compression event, relativelyfast rates of heat transfer out of the gas near TDC compression canresult in cooler in-cylinder contents than if there were no heattransfer at all. Also, mass flow rate decreased 7.5% due to heattransfer when comparing a normally firing cylinder with wall heattransfer to a firing cylinder with adiabatic walls, primarily due to thedensity effect.

Referring to FIG. 9, with respect to the effect of wall temperatures,i.e. piston temperature, head temperature, and liner temperature, on theSOC, Applicants have determined that as wall temperatures are increased,SOC becomes more advanced. The increased surface temperatures causelower heat transfer to the combustion chamber surfaces thereby advancingcombustion. Applicants have shown that with wall temperature varyingfrom 255 to 933 K and all other parameters kept constant (IMT=342 K,reheat=43 K, φ=0.24), the mixture did not ignite with a wall temperaturebelow 400 K. From about 400 K to 550 K combustion duration increases asa larger percent of the fuel burns. Above 550 K all the fuel burns andthe combustion duration decreases with increasing temperature. Varyingin-cylinder surface temperatures can be achieved by varying the coolingeffect of the engine coolant and/or the lubricating oil on thecylinder/piston assembly. Although cylinder wall temperature may bedifficult to use as a lever for effectively controlling SOC, cylinderwall temperatures are one of the parameters considered when controllingSOC, particularly for starting or transient operation. Applicants haveshown that there is a region of operating conditions where there are twostable solutions: one without combustion and cool walls, and one withcombustion and hot walls. Also, varying the surface to volume ratio inthe combustion chamber can change the heat transfer and, therefore, canbe used to control the combustion.

By comparing a normally firing cylinder with wall heat transfer to afiring cylinder with adiabatic walls, wall heat transfer is seen to bethe major contributor to spatial temperature distribution at TDC.Spatial temperature distribution is defined as the manner in which thetemperature varies throughout a region, be it in the port, or in thecylinder at a particular crank angle. By varying the in-cylindertemperature distribution, the start of combustion and/or the overallcombustion rate can be positively affected. One way to vary in-cylindertemperature distribution is to use split intake ports arranged so thatsome of the incoming air/fuel mixture is warmer/colder than the rest ofthe incoming mixture. Another method is to introduce hot spots in thecylinder or to use a glow plug 44 (FIG. 1a). Also, in-cylindertemperature distribution may be controlled by varying the temperature ofthe combustion chamber walls (e.g. the wall temperature of the cylinderliner, piston and/or engine head) by varying, for example, thetemperature of the engine coolant, the temperature of the engine oil orthe rate of cooling of the combustion chamber walls. As shown in FIG.1b, the temperature of the engine coolant may be varied by controllingthe flow through a coolant heat exchanger 46 positioned in the enginecoolant circuit 47 by varying the flow through a bypass circuit 48 usinga bypass valve 50. It was determined that wall heat transfer has similarimpact on spatial temperature distribution for both firing and misfiringcylinders. Similarly, applicants also determined how residualtemperature and wall heat transfer affect in-cylinder temperaturedistribution throughout intake and compression. The determinationincluded three studies of the intake and compression events of an airand propane mixture. These studies revealed that, during most of intakeand compression, hot residual is the main source of spatial temperaturevariation. However, near TDC compression, residual history is of minorimportance compared to heat transfer with the walls in setting uptemperature variations in the combustion chamber. As a result, it isbelieved that to promote a combustion event that uses more of the fuelthat is available, fuel may be introduced in such a way that at SOC,fuel and air exist in proper proportion in regions where the temperaturefield is adequate to sustain combustion. Two areas where the temperaturefield is inadequate to sustain combustion are in the crevices andadjacent cooled surfaces. It is therefore desirable to keep the fuelaway from both the crevices and cooled surfaces.

Clearly, heat transfer into the in-cylinder mixture increases thetemperature of the in-cylinder mixture thus advancing SOC. Applicantshave shown that a glow plug can be used to effectively control the SOCto a small degree. As shown in FIG. 10, once the glow plug is turnedoff, the SOC and EOC retard slightly. Also, GIMEP decreasessignificantly since less fuel is being burned. The decrease in theamount of fuel being burned also results in a decrease in the heatrelease rate as shown in FIG. 11. Between cycles #1 and #100, the glowplug was turned off and remained off until a time between cycles #300and #400, at which point it was turned back on. Perhaps mostimportantly, when the glow plug is turned off, the start of rapidcombustion is significantly delayed without an increase in duration,which in combination with the decrease in heat release rate, causes thecumulative heat release to decrease. Thus, glow plug 44 (FIG. 1b) couldbe used to positively control combustion to a limited degree.

In any practical reciprocating engine, heat will be lost from thecombustion chamber during the compression process. The heat loss dependsupon many factors, but primarily upon engine speed and the temperaturedifference between inside and the outside of the cylinder. This heattransfer during the compression process becomes a problem for dieselengines during cold ambient starts as combustion can be difficult toinitiate and sustain in cylinders where the combustion chamber surfacesare cold. Typically, the cylinders located at the ends of each bank ofcylinders run the coldest and are the least likely to fire. It is quitecommon under such conditions for the charge in the end cylinders to failto combust due to excessive heat exchange with the colder cylinderwalls. With diesel engines, however, once all the cylinders warm up,combustion is quite consistent and much less dependent on combustionchamber surface temperatures.

With PCCI, the combustion process is initiated by obtaining a certainpressure and temperature “history”. Thus, as discussed hereinabove, thePCCI combustion process is strongly dependent upon, and sensitive to,the surface temperatures of the combustion chamber. The present PCCIengine may include an end cylinder compensating means for achievingdesired combustion chamber surface temperatures in the end cylinders toensure better cylinder-to-cylinder temperature control therebyincreasing the likelihood of stable combustion and very low NOxemissions. The end cylinder compensating means may include a system forreducing the effective cooling of specific cylinders, such as reducingpiston cooling nozzle flow; increasing coolant temperature; or reducingcoolant flow rate. Specifically, referring to FIG. 12, the end cylindercompensating means may include an oil flow control system 70 includingoil flow control valves 72 positioned in branch flow passages 74delivering cooling oil to piston cooling nozzles 76 from an oil pump 78.Thus, control valves 72 can be controlled to vary the flow of coolingoil to the piston assemblies to vary the temperature of the piston andthus favorably influence the in-cylinder temperature. Alternatively,flow restrictions could be used instead of valves 72, or the nozzles 76associated with the end cylinders may be designed with a smallereffective flow area than the remaining nozzles to permanently reduce theflow to these piston cooling nozzles. In addition, if more than onenozzle 76 is provided as shown in FIG. 1a, the number of nozzlesoperating could be varied by controlling the respective control valvesassociated with each nozzle.

Referring to FIG. 13, end cylinder compensating means may include anengine coolant flow control system 80 including a coolant pump 81 andcoolant flow control valves or restrictions 82 positioned in branchpassages 84 leading to the end cylinders 86 of the engine 88. The valves82 are operated to reduce the flow of cold coolant delivered from aradiator 90. Also, control valves 92, positioned in hot coolant returnpassages 94, are used to control the flow of higher temperature coolant,bypassing radiator 90, and delivered directly to the end cylinders.These systems all function to control the flow of coolant to the endcylinders to compensate for the fact that they are cooled more by theambient surroundings so that the total cooling to each end cylinder isequal to each of the other cylinders. These systems can be used toassist in cylinder warm-up to improve engine startability and to provideenhanced control of cylinder combustion and cylinder-to-cylinderbalancing.

The end cylinder compensating means may, alternatively, or additionally,include end cylinders having an effective compression ratio nominallygreater than the other cylinders to offset the extra heat loss. Thiscompression ratio could be designed into the end cylinders so that theend cylinder compression temperature is equal to the middle cylinders.This approach is advantageous from a performance perspective since endcylinder combustion chamber surface temperatures would be enhanced forboth start-up as well as warmed-up operation. This compression ratiodifference may alternatively be accomplished through the camshaft valvelobe phasing. In this scenario, the end cylinders would have intakevalve closing (IVC) near bottom dead center (BDC) so that the effectivecompression ratio (CR) is approximately equal to the geometric CR. Themiddle cylinders could then have a retarded IVC which would produce alower nominal effective CR than the end cylinders. The effect of varyingthe compression ratio on PCCI combustion is discussed more fullyhereinbelow.

One of the biggest challenges with premixed charge, compression ignition(PCCI) engine technology is in the placement of the heat releaseprofile. Start of combustion with standard diesel or spark ignitionengines is controlled with injection timing or spark timing. With PCCIengines, the start of combustion is dictated by the in-cylindertemperatures and pressures. As SOC timings near TDC (and after) areapproached on the PCCI engine, the sensitivity to small geometric and/oroperational variations in temperatures, pressures, etc. increasedramatically. As retarded heat release profiles are sought for PCCIengines (to minimize peak cylinder pressures and improve efficiency),the risk of misfire or partial burn increases dramatically. This is dueto the fact that the cylinder temperatures decrease after top deadcenter due to the expansion of the charge. If autoignition has not yetoccurred by TDC, autoignition will not likely occur much after top deadcenter. This problem is further aggravated if one cylinder begins tomisfire. The misfiring cylinder cools down making it even more likelythat the misfiring will continue.

In a multi-cylinder engine variations inevitably exist between cylinderswith respect to compression ratio, wall temperatures, reheat andresidual mass fraction. This variability makes it quite difficult tooperate a PCCI engine with the desired retarded combustion timing whilemaintaining optimum combustion without having individual cylinders(which happen to be running slightly cool) begin to misfire.

Applicants have determined that manipulating valve events can have asignificant effect on the temperature at TDC and therefore is aneffective tool for controlling the start of combustion as suggested byanalytical results shown in FIG. 14. Specifically, referring to Table I,varying valve events has the following effects:

TABLE I effect of advancing effect of retarding modified valve timingrelative to valve timing relative event baseline baseline to baselineEVC −357° traps hot residual which exhaust blown back advances SOC intointake which advances SOC EVO   135° no effect no effect IVC −167°Miller cycle - lowers at these particular effective CR which conditions,retarding retards SOC slightly improves breathing; retarding furtherreduces effective CR which retards SOC IVO   341° allow hot exhaust torestricts flow from flow into intake which intake manifold whichadvances SOC has minimal effect on SOC

As shown in FIG. 15, exhaust valve closing (EVC) plays a significantrole in determining the amount of combustion products that remain in, orare made available to, the combustion chamber from one combustion eventto the next event, i.e. the residual mass fraction (RMF). The residualexists at a higher temperature than the incoming charge and thereforeheats the charge for the next combustion event. Thus, the timing ofexhaust valve closing can be used to adjust the in-cylinder temperatureand therefore controlling the SOC. In order to “heat up” a cold cylinder(e.g. one that is beginning to misfire) the residual mass fraction canbe increased in the individual cylinder by an early exhaust valveclosing event. These hot residuals will increase the reheat of theincoming charge and tend to advance the start of combustion thereby, forexample, restoring a misfiring cylinder. As shown in FIG. 15, advancingEVC traps hot residual in the cylinder while retarding EVC allows hotexhaust to be blown back into the cylinder (in this case, exhaustmanifold pressure (EMP)>IMP). The baseline EVC is the optimum of thesetwo effects: trapping the minimum amount of residual and resulting inthe lowest TDC temperature. Similarly, advancing IVO allows some of thehot residual in the cylinder to be blown back in to the intake, againbecause EMP>IMP, causing the TDC temperature to increase. Loweringcompression ratio, discussed more fully hereinbelow, by, for example,advancing IVC, will also increase residual in the cylinder, but to alesser extent. Adjusting the timing of exhaust valve closing may also beused to effectively compensate for the small geometric and operationalvariations between the cylinders to permit the engine to be “tuned”cylinder-to-cylinder. Any other means for effectively increasing ordecreasing the RMF may be used to advance or retard the SOC,respectively.

One method of implementing this strategy has been successfully tested ona multi-cylinder PCCI engine. This technique involved the increase ofthe exhaust valve lash setting. Opening up the lash effectively closesthe exhaust valve early and advances the start of combustion as desired.Applicants have determined that reducing the exhaust valve event by 10degrees leads to slightly higher surface temperatures and 22 degreewarmer inlet temperatures. Given the dramatic effect that 22 degree IMTswings have on combustion (FIGS. 7c-7 f), this method would indicate apotential for tuning the multi-cylinder engine with valve lashadjustments. As shown in FIG. 16, shortening the duration that anexhaust valve is open by increasing the lash does indeed advancecombustion. Ultimately, cylinder-to-cylinder variations can becontrolled passively by any means which can adjust the static exhaustvalve closing. It could also be controlled actively if it is coupledwith some diagnostic measurements. If control exists on all cylindersthen this technique could also be used to effect the overall start ofcombustion within the engine.

Another method of controlling in-cylinder temperature by controlling theresidual mass fraction (RMF) is to compress a pocket of residual gasfrom the previous cycle in a chamber positioned separate from theincoming charge. The proportion of trapped residual to fresh charge canbe manipulated by the size of such a chamber. The mass of hot exhaustcould be as large as (½)(1/CR) and therefore ≈{fraction (1/30)} of thechamber mass if all the TDC volume is in such a chamber. The structureof such a chamber will have to be managed to make at least a portion ofthe hot gas survive the compression process without completely mixingwith the incoming charge. If the trapped exhaust is mixed very early inthe compression process, the high temperature required to initiate thefast reactions will not be reached. The timing of flows into and out ofsuch a chamber may help manage the timing of the beginning of rapidenergy release in cylinder. Additional sources of local heat input maybe able to supply such a fast reaction initiation. This might be aheated glow plug or a thermally isolated mass.

The residual mass fraction is also sensitive to the exhaust manifoldback pressure (EMP). By increasing EMP relative to IMP, the residualmass fraction can be increased thus increasing the temperature of thecharge which, in turn, advances combustion. Applicants have determinedthat raising EMP does have the expected result of advancing SOC.However, applicant also showed that SOC advanced only by about 4° with a3 bar increase in EMP for a four cycle engine. Applicants havedetermined that the increase in temperature is nearly linear withincrease in EMP, with all other things being held constant. For a 1 barincrease in EMP, temperature at TDC increased about 10 K. Therefore,considering the practical range of EMP, controlling EMP seems to be arelatively weak lever in controlling SOC on a four cycle engine.Moreover, a very substantial BSFC penalty is paid when using EMP toincrease TDC temperature in a four cycle engine. The BSFC would besignificantly higher than using either exhaust valve closing or variablecompression ratio. Although the effect of increasing EMP is the same asadvancing EVC, i.e. trapping more hot residual mass in the cylinder, theBSFC is much higher because, when EMP is increased, the piston has towork against that pressure through the entire exhaust stroke. If theengine has turbomachinery, then further complications would arise withtrying to use EMP to control SOC. However, using an exhaust restrictionmay still be viable on a two-cycle engine.

Another important way to control intake temperature is by using hotexhaust gas recirculation (EGR). As shown in FIG. 1b, a high pressureEGR circuit 54 may be used to direct hot exhaust gas from upstream ofturbine 25 into the intake system 23. EGR circuit 54 includes a highpressure EGR control valve 60 for controlling the recirculation ofexhaust gas. A low pressure EGR circuit 62 and control valve 64 may beused to direct a flow of low pressure EGR from downstream of turbine 25into the intake system 23. Applicants have shown that EGR is especiallyeffective in increasing the intake manifold temperature when introducedupstream of the compressor 24 (assuming the effect of adding EGR is notcancelled by additional charge air cooling). Exhaust gas recirculation(EGR) has more utility in PCCI engines because the exhaust gas of suchan engine will contain less particulates and thus the exhaust gas can berecirculated to the ideal upstream location (intake of compressor ofturbocharger). The intake of the compressor is the best location becausethe pressure differential is almost always favorable. The fresh intakeair and hot EGR mixture will get compressed by the compressor therebyproviding heating and mixing. By introducing the EGR upstream of thecompressor and increasing the compressor inlet temperature, the resultis a much higher compressor outlet temperature than if the EGR isintroduced after the compressor. Introducing EGR into the intake of thecompressor is very difficult in normal diesel engines because theparticulates in the exhaust gases of the engine “gum up” the compressor.In a PCCI engine, however, the virtually particulate free exhaust couldbe introduced upstream of the compressor without significant problems.Also, as shown in FIGS. 16, 17 and 18, applicants have determined that,regardless of the technique used to introduce exhaust products, e.g.EGR, RMF, etc., by adding exhaust products while maintaining thetemperature of the charge by, for example, injecting a cooling diluent,such as air and/or water, the combustion rate can be slowed thusincreasing the combustion duration, retarding combustion and decreasingthe amount of heat release.

Referring to FIG. 19, an improved engine 100 is shown which benefitsfrom the PCCI engine and control system of the present invention byoperating a limited number of a plurality of cylinders in a PCCI modewhile operating the remainder of the cylinders in a diesel mode.Specifically, for example, five cylinders 102 in a six cylinder enginemay be operated in the diesel mode while one cylinder 104 is operated ina PCCI mode. This engine also includes an EGR system 106 associated onlywith the PCCI cylinder 104 and separate from an exhaust system 108associated with the diesel cylinders 102. The pressure of the piston inthe PCCI cylinder 104 is used to force the exhaust gas into the intakesystem. The EGR system 106 includes an EGR cooler 110 utilizing, forexample, engine coolant, which cools PCCI exhaust gas beforerecirculating the gas to the upstream side of a compressor 105. Ofcourse, the exhaust gas could be delivered to the intake manifold 112serving only diesel cylinders 102. A well known problem confronted inthe use of EGR in diesel engines is the excessive amounts ofparticulates and NOx present in diesel engine exhaust gas. The improvedengine 100 permits a diesel engine to benefit from EGR whilesubstantially avoiding the drawbacks associated with heavy particulatediesel exhaust thereby providing a less complex and costly system. Forexample, as discussed hereinabove, the PCCI EGR from cylinder 104 couldmore easily be introduced upstream of the compressor without fouling thecompressor. Also, the low NOx emissions of the PCCI EGR reduce theformation nitric acid thereby reducing corrosion in the engine.Applicants have shown that the engine of FIG. 19 lowers the brakespecific NOx emissions while only negligibly increasing the brakespecific fuel consumption.

Perhaps one of the most effective control features for varying thetemperature at TDC and therefore the SOC is variable control of thecompression ratio (CR) of a cylinder. By varying the effective or thegeometric compression ratio, both the temperature and the pressurehistories can be controlled. Increasing the compression ratio advancesthe combustion event. Decreasing the compression ratio retards it. Forcertain purposes, the compression ratio may range from 24:1 (to promotecold starting) to 12:1 (to permit control over the start of combustionand limit the peak combustion pressures). The range of compressionratios would depend on, among other factors, the type of fuel used (morespecifically its autoignition properties), for example, natural gas orpropane. Applicants have determined the effect of compression ratio onPCCI combustion. For example, referring to FIG. 20, applicants haveshown that varying the compression ratio is a large lever in changingin-cylinder temperature and therefore SOC. As shown in FIG. 21,applicants have shown that variations in compression ratio significantlyaffects the location of the SOC relative to TDC.

The compression ratio can be varied by varying the geometric compressionratio, i.e. using a control mechanism to vary the physicaldimensions/shape of the combustion chamber. The present inventionincludes a compression ratio varying device 38 for varying the geometricor the effective volume of the combustion chamber during engineoperation to achieve a desired SOC. The compression ratio varying devicemay be a mechanical device for causing compression heating of the chargenear TDC by changing the geometric volume of the combustion chamber. Asshown in FIGS. 22a-22 d, the compression ratio varying device mayinclude a movable auxiliary piston or plunger which moves to extend intothe combustion chamber at a crank angle near TDC to decrease thecombustion chamber volume thereby increasing the compression ratio andheating the charge sufficiently to allow ignition to start. The keyfunction of the plunger is to displace some of the charge near TDC.Therefore, the shape and location of the plunger in the combustionchamber will not be critical to its function, except to the extent thatthe plunger affects the crevice volume.

The size of the plunger will be based on the desired compression ratiocontrol range and may be estimated by the following example:

Swept volume (displacement) per cylinder=1,000 cc=1 l.

TDC clearance volume=100 cc

Compression ratio=(1000 cc+100 cc)/100.0 cc=11.0

If the plunger volume=30 cc, then the effective compression ratio withplunger fully extended=(1000 cc+100 cc)/(100 cc−30 cc)=15.7.

For a given set of conditions, the modified compression ratio should besufficient to allow a large enough increase in temperature and pressureto cause compression ignition for a fuel/air mixture that would notignite without the plunger. Of course, the engine's compression ratioand the size of the plunger are easily changed during the design stageof the engine. Also, different fuels and intake temperatures couldrequire different plunger sizes and compression ratios.

As shown in FIG. 22a, the plunger 150 may be positioned in a bore 152 inthe cylinder head 154 and operated by a cam 156 rotated in predeterminedtimed relationship to the movement of the engine piston 158. Aretraction spring 160 biases the plunger toward cam 156 to increase thesize of combustion chamber 162. This particular arrangement isadvantageous in that cam driven plunger 150 can put work back into thecamshaft as the plunger retracts. Also, some of the work that plunger150 does on the charge can be extracted by the engine piston, as long asplunger 150 does not retract until late in the expansion stroke, orafter the expansion stroke.

Alternatively, referring to FIG. 22b, a plunger 170 may be hydraulicallyoperated by a pressurized supply of fluid, e.g. fuel, delivered to achamber 174 by a hydraulic circuit 172 connected to, for example, a jerkpump or common rail system. FIG. 22c, illustrates another hydraulicallyactuated embodiment in which a plunger 180 is assisted by a spring 182,positioned in a chamber 184 formed adjacent one end of plunger 180, toallow energy to be stored in the spring. In this system a retainingmechanism, e.g. hydraulic, electromagnetic or mechanical, (not shown)maintains the plunger in the unextended position. When the piston isnear TDC, a hydraulic fluid supply system 186 forces plunger 180 down(at this point the retaining system no longer holds the plunger). Thisdownward motion is heavily assisted by spring 182. After combustion,plunger 180 moves back up recompressing spring 182 thereby returningenergy to the spring. To optimize this energy extraction process, thehydraulic chamber 184 bleeds down at a rate controlled by a valve 188.

FIG. 22d illustrates yet another embodiment in which a spring 190,biasing a plunger 192 into the extended position, is strong enough toovercome the gas pressure in the combustion chamber before combustion.Near TDC, a bleed down valve 194, connecting a chamber 196 is opened andthe spring 190 pushes plunger 192 into the extended position in thecombustion chamber 162 causing the charge to ignite and the pressure inthe combustion chamber 162 to increase. As a result, plunger 192 ispushed back up against spring 190. If needed, a high pressure supply 200supplies hydraulic fluid to chamber 196 to ensure plunger 192 moves backup into the retracted position. If the gas pressure is sufficient tomove the plunger back up into the retracted position, a low pressurehydraulic fill supply 202, including a one-way valve 204, may be used tofill the chamber 196 below plunger 192.

The compression ratio may also be varied by providing an opposed pistonengine design having variable phase shifting to permit the compressionratio to be varied during operation by changing the phase of rotationbetween two crankshafts. The opposed piston engine may be of the typedisclosed in U.S. Pat. No. 4,010,611 or of the interconnected cylindertype with variable phasing as disclosed in U.S. Pat. No. 4,955,328, theentire contents of both of these references being hereby incorporated byreference. Alternatively, referring to FIG. 23, the compression ratiocould be varied using a phase shifting mechanism 210 including aconventional differential assembly 211 connected between an input shaftportion 212 of one of the crankshafts 214, 216 associated withrespective pistons 218, 220 and an output shaft portion 222 of the samecrankshaft 214 to permit the portions of the crankshaft to be rotativelyshifted relative to one another. Crankshafts 214 and 216 are connectedvia a conventional gear assembly 223 for transferring power to a drivenshaft 225. As shown in FIG. 24, the differential 211 includes a ringgear 224 mounted on one end of input shaft portion 212, an arm 226extending from ring gear 224 and a gear assembly 227 mounted on theopposing ends of shafts portions 212, 222. A rotator mechanism 228,including a pinion gear 230, is operatively connected to ring gear 224to rotate the ring gear when a change in the phasing between thecrankshafts is desired. As long as ring gear 224 remains stationary,shafts portions 212, 222 remain in phase. When ring gear 224 is rotatedby rotating pinion gear 230, arm 226 rotates causing a change in thephasing between shaft portions 212, 222. The rotator mechanism 228would, therefore, be used to adjust the relative phasing of the inputshaft to the output shaft, thereby adjusting the phasing of the twocrankshafts and the compression ratio. In addition, two crankshafts percylinder could be used to eliminate the inherent side thrust imparted bythe crankarm in the single crankshaft design. The effect of the maximumpossible compression ratio on the sensitivity to CR on phasing should benoted. It might be advantageous to have a geometry where the pistonsinterfere with each other at “zero” phasing. Of course, this set upwould operate with non-zero phasing all the time.

Applicants have determined how the change in phasing of an opposedpiston engine changes the compression ratio. This effort includes threestudies as shown in FIG. 25. In the first, when the two pistons were inphase, i.e. both pistons reach TDC at the same time, the compressionratio was 25:1. In the second, when the pistons were in phase they wouldcome together and just touch at TDC. With a flat top piston there wouldbe no volume between the pistons and, assuming no crevice volume, thecompression ratio would become infinite. The third case assumes negativeinterference so that the pistons would come in contact while out ofphase to some degree. For this case, the overlap was about 10% of thestroke causing the pistons to contact at 46° out of phase. Of course,engine geometry (bore, stroke, connecting rod length) will also effectCR versus phasing; these values were kept constant in this study.

These results indicate that the compression ratio could be varied over avery large range using an opposed piston arrangement with variablephasing. Also, the slope of the change in compression ratio with phasingdepends on the amount of clearance or negative clearance between thepistons at TDC with 0° phasing. Thus, in a practical application, itwould be desirable to strike a balance between the range of phasingneeded to cover the desired range of compression ratio and the precisionwith which the phasing needs to be controlled, i.e. the slope of thecurve in FIG. 25 should be optimized. Thus, ideally, the slope of thecurve would be steep enough that the desired range of compression ratiocould be achieved within a limited amount of phasing, and not so steepthat the phasing needs to be too precise.

Referring to FIG. 26, it is very clear that as the pistons become moreand more out of phase that the compression ratio decreases. It is alsoclear that there is very little change in shape of the cylinder volumeversus crank angle curve for phasing angles less than about 120°. As aresult, the variation in phasing can be used to control compressionratio over a large range without any affect in the cylinder volumeversus crank angle. An opposed piston system with variable phasingclearly provides the desired flexibility to achieve a broad range ofcompression ratio values.

The effective compression ratio may be varied with variable valvetiming. Specifically, as shown in Table I, advancing of the intake valveclosing lowers the effective CR while significant retarding of the IVCalso reduces effective CR. However, changing valve events can have avery large effect on the breathing of an engine, and thus the air/fuelratio, in comparison to varying the geometric compression ratio(assuming that the fuel flow rate is held constant). The steepest changein airflow with TDC temperature is when IVC is changed. As IVC becomesearlier, the TDC temperature is lowered, but airflow is severelyrestricted possibly undesirably changing the equivalence ratio. In thiscase, an increase in boost accompanying earlier IVC could be used tomaintain a constant air flow rate. Similarly with EVC, as EVC is changedthe amount of residual trapped in cylinder changes, and thereforebreathing is affected. The slope of the IVC line is roughly twice thatof EVC and IVO while varying the geometric compression ratio does nothave an effect on airflow. In terms of changing TDC temperature withouteffecting airflow, variable geometric compression ratio appears to bethe most effective of the control features.

Referring to FIG. 28, changing any of the valve events or compressionratio has a definite effect on BSFC. In order to get the best BSFC,increasing compression ratio would be a better choice than changingexhaust valve closing when a higher temperature is needed. A very largeBSFC penalty would be paid if EVC is advanced to increase thetemperature at TDC. If a lower temperature is needed, advancing IVC isthe best method whereas varying the geometric compression ratio couldalso be an option since it results in only somewhat higher BSFC.

Applicants have also determined, as expected, that changing theeffective compression ratio has a large effect on peak cylinderpressure, as shown in FIG. 29. IVC has an almost identical curve as VCR,confirming the fact that changing IVC really changes the effectivecompression ratio. Because the heat release starts 5° ATDC in this case,the cylinder pressure trace appears to be “double-humped”: the firstpeak at TDC is due to compression; the second peak after TDC is due tocombustion. The appearance of two slopes of VCR and IVC lines is due tothe absolute peak cylinder pressure occurring either on the combustionhump (CR<18) or the compression hump (CR>18). In order to increase thetemperature at TDC from the baseline without undesirably affecting peakcylinder pressure, changing EVC or IVO would be the best strategy.However, this strategy may result in an undesirable increase in BSFC(FIG. 28) and may also change the engine breathing (FIG. 27).

Applicants have also determined that very high compression ratios areneeded for combustion at low intake temperatures. For example, it hasbeen found that at intake temperatures of 0, 20, and 40° F., nocombustion occurs when the corresponding compression ratios are below35, 33, and 30, respectively. At warmed up conditions, the desiredcompression ratio is approximately 15, which means that a change ofapproximately 20 compression ratios would be needed to cover theseconditions. Due to the very high compression ratios required under theseconditions, peak cylinder pressures are also high and in some casesgreater than 200 bar. As a result, intake air heaters and/or some othermethod of starting in cold conditions may be more practical than usingvariable compression ratio alone. Also, maintaining a lower compressionratio will allow a higher GIMEP to be achieved before hitting the peakcylinder pressure limit.

Another method of controlling the temperature is to introduce water intothe intake manifold or directly into the cylinder. Applicants have shownthat when the nitrogen in the intake air is completely replaced withwater, the water will likely result in a lower flame temperature (205 Klower) due to dissociation. Also, in applicants study, the ignitiondelay increased slightly (by 0.04 msec) and the peak reaction ratedropped by about 50%. Also, when water was added into the intakemanifold, e.g. water fumigation, the chemical effect, although small, isto slightly retard the SOC. However, liquid water injection into theintake manifold effectively cools the intake manifold due to thevaporization of the liquid to steam. As a result, IMT and TDCtemperatures are significantly decreased as shown in FIG. 30. The impactof water injection on temperature at TDC is mostly due to the decreasein IMT, not due to the change in the ratio of specific heats. The effecton IMT should be viewed as an upper limit.

It should be noted that applicants have shown that PCCI can bemaintained without adverse thermal effects on the piston 14 (FIG. 1a).Even though PCCI combustion can create knock intensity levels 10-20times higher than the safe level experienced in spark-ignited engines,both aluminum and steel pistons do not reach excessive temperaturelevels. In applicants' preferred embodiment, the temperatures resultingfrom autoignition in PCCI combustion are much lower than thetemperatures experienced in spark-ignited engines since, in applicants'preferred embodiment, PCCI combustion operates under such leanconditions.

Pressure Control

The SOC may also be controlled by controlling the pressure in thecombustion chamber. One way of controlling in-cylinder pressure is touse a compression ratio varying device to vary the pressure in thecombustion chamber. Although varying the compression ratio ultimatelyvaries both the pressure and temperature of the charge, the pressure isdirectly changed. An increase in the compression ratio will tend toincrease the pressure at TDC, and a decrease in compression ratio willdecrease pressure at TDC. Applicants have shown that increasing thein-cylinder pressure advances the start of combustion and decreasing thein-cylinder pressure retards the SOC. Any of the compression ratiovarying devices discussed hereinabove with respect to temperaturecontrol may be used.

A second way of controlling the in-cylinder pressure is to vary to theintake manifold, or boost, pressure (IMP). The timing of the SOC hasbeen shown to be a function of pressure. Applicants have determined theeffects of varying IMP on combustion and engine operation. The engineconditions for one engine study were 1200 RPM, 355.7 K<IMT<357.4 K,0.256<φ<0.263. IMP was varied. Maintaining these conditions whileincreasing IMP required increasing air flow and fuel flow. FIGS. 31a and31 b show that the duration of heat release decreases as IMP increasesboth in the crank angle domain and the time domain. FIG. 31d shows thatSOC occurs earlier as IMP increases. FIG. 31c, showing results fromanother study, clearly indicates that increasing the boost pressuresignificantly advances the heat release event. FIG. 31e shows that FSHCemissions decrease as IMP increases, indicating more completecombustion. FIG. 31f shows that GIMEP increases as IMP increases, mostlydue to the increase in complete combustion, and, to a lesser extent,more fuel. FIG. 31g shows that gross indicated thermal efficiencyincreases as IMP increases, partly due to more complete combustion. FIG.31h shows that FSCO emissions decrease as IMP increases, apparently dueto more complete combustion. FIG. 31i shows that FSNOx emissions are notsignificantly affected by IMP. FIG. 31j shows that coefficient ofvariation (COV) of GIMEP decreases as IMP increases. FIG. 31k shows thatPCP increases as IMP increases. FIG. 31l shows that estimated noiseincreases as IMP increases. FIG. 31m shows that as IMP increases,smaller gains in GIMEP cause larger rises in PCP. This effect is due tothe earlier SOC that occurs as IMP increases.

One study varied the pressure at BDC of the compression stroke. Thestudy was performed using a compression ratio of 14.5:1, an engine speedof 1200 rpm, a BDC compression temperature of 389 K, an equivalenceratio of 0.3285, and no heat transfer. The fuel used was propane and thepressure at BDC was varied while all other parameters were heldconstant. This study clearly revealed that as pressure at BDCincreases,the SOC becomes earlier. In addition, for BDC pressures lessthan 1.75 bar, less than 10% of the fuel energy was released, while forBDC pressures greater than P=1.75 bar, virtually all of the fuel energywas released. This indicates that the combustion is highly sensitive tochanges in pressure. At very low pressures, very little of the fuelburns, leading to high FSHC emissions. Since none of the fuel is burningat these low pressures, no carbon monoxide is produced. As the pressureincreases (while maintaining IMT constant), a higher percentage of thefuel is burned, which leads to decreased production of carbon monoxideand lower FSHC. Above a certain critical pressure, all of the fuel burnscompletely, leading to extremely low FSHC and FSCO emissions. Also, avery small change in BDC pressure leads to a very large change in peakcycle temperature (PCT). The results of the simulation indicate that atlow peak cycle pressures (PCP), the fuel does not burn. Hence, thepressure peaks at the isentropic compression. As pressure is increased,a higher percentage of the fuel energy is released, causing the cylinderpressure to rise above the isentropic compression pressure. As pressureincreases further, all of the fuel energy is being released and furtherincreases in pressure raise the PCP due to isentropic effects.

Clearly, varying IMP can be an effective way of controlling the SOC andthe duration of combustion. Increasing the IMP tends to advance SOCwhile decreasing the duration of heat release. Likewise, decreasing theIMP tends to retard SOC while increasing the duration of heat release.In a typical application, for a constant torque condition, the fuel flowrate would remain virtually constant, and the boost pressure would beincreased to advance the start of combustion or decrease the boost toretard the start of combustion. For example, an air compressor, aturbocharger, a supercharger such as driven by an engine power take-off,or an electrically powered compressor, could be used. For a given powerlevel, and, therefore, for a given fuel flow rate, there typicallyexists a preferred intake pressure and temperature. At very low loads,it may be desirable to control the intake manifold pressure with athrottle 53 (FIG. 1a) in the same way that the intake pressure iscontrolled on a current production spark ignited engine. Throttle 53would also be used when operating a multi-mode PCCI engine in a sparkignited mode as described hereinbelow. Of course, a throttle couldalternatively be located at other locations in the intake system, suchas in the intake manifold.

Air/Fuel Mixture Autoignition Properties

Another strategy for controlling the start and duration of combustion isto vary the air/fuel mixture autoignition properties. The autoignitionproperties of the air/fuel mixture may be controlled by injecting a gas,e.g. air, oxygen, nitrogen, ozone, carbon dioxide, exhaust gas, etc.,into the air or air/fuel mixture either in the intake system, e.g.preferably in the port using, for example, injector 42, or in thecylinder directly using, for example, injector 40, thereby providingcontrol over the start of combustion and the combustion rate.

Applicants have examined the effect of adding reactive species to theair/fuel mixture on the combustion process. One study was performedusing an equivalence ratio of 0.3, a temperature at BDC of 389 K,pressure at BDC of 3 bar, and propane as the fuel. The compression ratiowas 14.5, and the engine speed was 1800 RPM. The engine geometry usedwas for a Cummins C series engine. The nitrogen, oxygen, and fuel molefractions were held constant at 0.771, 0.216, and 0.0123, respectively,for all cases. The mole fraction for the reactive species added was0.000411 for all cases. The reactive species examined were H₂, H₂O₂, OH,CO, O, HO₂, H, and O₃. FIG. 32 shows the temperature versus crank angle.Although CO and H₂ advanced the SOC by less than 0.5 crank angledegrees, all other species significantly advanced the SOC, with O₃(ozone) causing the largest change in the SOC. Therefore, smallconcentrations of most common radicals will cause significant changes inthe SOC.

Thus, applicants have determined that the addition of very smallquantities of ozone advances the SOC by significant amounts. Applicantshave also shown that virtually all of the ozone will be consumed by thecombustion process and that the change in the SOC will diminish as theamount of ozone added increases. Specifically, FIG. 33 illustrates theeffects of additional ozone on advancing the SOC. The increase intemperature indicates the start of the combustion event.

Given the significant effect additional ozone has on the SOC, ozone canbe used in several ways to advantageously control the combustion in aPCCI engine. First, by adding different amounts of O₃ to the intakeports, one, several, or all cylinders could have their SOC adjusted.Second, adding O₃ to the intake could be used as a cold starting aid forPCCI and diesel engines. Third, adding O₃ to the exhaust of an enginewould allow a catalyst to light earlier thus possibly significantlyreducing cold start emissions on catalyst-equipped spark ignitedengines, diesel engines and PCCI engines. O₃ could be produced “onboard” through a simple electro-chemical reaction. Ozone generators arecommercially available. Also, the ignition delay of a diesel enginecould be reduced by adding O₃ to the intake. This would reduce thepremixed burn fraction which would then lower NOx emissions and reducednoise.

Applicants have shown that increasing the oxygen concentration advancesthe SOC. However, applicants have determined that oxygen enrichment from20.7 percent to 21.65 percent will advance the SOC by less than onecrank angle degree, and oxygen enrichment from 20.7 percent to 23.7percent will advance the SOC by less than 1.5 crank angle degrees.Therefore, combustion may be controlled to a limited degree by modifyingthe oxygen concentration of the intake air. This may be done by addingoxygen (or an oxygen rich gas mixture) to the intake or by selectivelyremoving nitrogen from the intake air (using a membrane for example).Applicants have also shown that increasing the percent of nitrogen inthe intake charge from 78.6 percent to 80.6 percent resulted in theretardation of the SOC by less than 2 crank angle degrees at 1800 rpm.It was also noted the same percentage increase of N₂ in the fresh chargelowers the FSNOx from 0.144 to .0.048 grams of NOx per Kg of fuel.

Another method of varying the effect of oxygen on the combustion processis to dilute the mixture with EGR. In one study, an engine EGR systemwas plumbed from the exhaust manifold to the compressor inlet. Becausethe EGR is mixed in upstream of the aftercooler, and in the presentstudy, the aftercooler exit temperature was controlled and held fixed,the EGR should not have significantly effected the temperature at SOC.During this study, fuel rate and intake manifold temperature were heldconstant. As the EGR rate was increased, exhaust manifold pressuredecreased, which in turn decreased air flow on this turbocharged engine.The fuel rate was held constant, so the fresh equivalence ratioincreased. In spite of the increased equivalence ratio, SOC retarded asthe EGR rate increased, most likely due to the diluent effect of theEGR. As expected, SOC retarded as the EGR rate increased. However, asEGR rate increased, CO and HC emissions also increased. Also, as EGRrate increased, the spread in SOC between cylinders increased. In asimilar study, the SOC was held constant by adjusting IMT. As the EGRrate was increased, exhaust manifold pressure decreased, which in turndecreased air flow. The fuel rate was held constant thus causing theequivalence ratio to increase. In addition, as the EGR rate increasedfrom about 7 to 13% EGR, there was a sharp rise in the cylinder tocylinder variation in SOC. Ultimately, a higher IMT was required tomaintain constant SOC as the EGR rate increased, in spite of an increasein equivalence ratio. This requirement was due to the diluent effect ofincreased EGR on the intake air.

Another technique for modifying the autoignition properties of theair/fuel mixture to control SOC and the duration of combustion is tovary the octane, methane or cetane number of the charge by, for example,by providing two or more fuels have different octane, methane or cetanenumbers. The fuel supply can be either selectively switched between thefuels or the fuels can be mixed. This technique makes it possible toretard or advance the combustion event. For example, a fuel which tendsto autoignite more readily (lower octane or methane number, or highercetane number) could be controllably mixed with a fuel that tends toautoignite less readily (or a fuel that ignites at a high temperatureand a fuel that ignites at a low temperature could be used) to enabledirect control over the timing of ignition and rate of combustion bychanging the ratio of the fuels that are present in the combustionchamber during the combustion event. As shown in FIG. 34, propane,octane and heptane have significantly different effects on the SOC. Thesame effect may be achieved by using a fuel additive, such as acontrolled amount of propane, ethane, or other hydrocarbons, such asengine lubricating oil, that change the autoignition properties of thefuel to advance or retard the start of combustion. Of course, any methodthat changes the fuel's octane/methane number or the activation energyof the fuel can be used to advance/retard combustion. Applicants havedetermined that there is a significant sensitivity of start ofcombustion to octane number. This effect was independent of intakemanifold temperature. Moreover, in one study, the start of combustionwas retarded approximately 7° for an increase in octane number from 80to 100.

Achieving dynamic control over individual cylinder combustion in amulti-cylinder PCCI engine will be critical to achieving improvedcombustion. Since many of the gases/fluids discussed hereinabove, e.g.fuel, ozone, oil, water, etc. have now been shown to significantlyaffect the SOC and/or rate of combustion, these additives can be used toadvantageously balance combustion between the cylinders in amulti-cylinder engine running on PCCI principles. For example, byinjecting a liquid or gas diluent, such as a less reactive fuel, water,uncooled or cooled exhaust products, air and/or nitrogen either into theintake air or directly into the charge in the cylinder, the SOC can beretarded. Also, by injecting, for example, a more reactive fuel, ozone,oil and/or oxygen into the charge the SOC can be advanced. FIG. 1billustrates one system for balancing combustion between cylinders of amulti-cylinder engine. The system uses port injection of fuel on theengine with two types of supplies per cylinder—supply 32 to injectliquid fuel and supply 34 to inject gaseous fuel. Although the supplies32 and 34 are shown feeding into a single passage for delivery to theintake port, the supplies may include separate delivery passagesconnected to the intake port at different locations. Liquid fuel willdecrease intake charge temperature by the heat of vaporization of theliquid fuel. The temperature at TDC compression, and therefore SOC, canbe controlled by varying the amount of liquid versus gaseous fuel. Also,it should not matter if the liquid vaporizes in the port or duringcompression. The gaseous and liquid fuel can be the same fuel indifferent states, e.g. propane, or different fuels, e.g. gaseous naturalgas and liquid gasoline, such as indolene. It is important that the portinjection system have good separation between cylinders and sequential(timed to intake event) injection is likely to be required. Duringoperation, a cylinder that is “going out” would be given more gaseousfuel and a cylinder that is “too hot” would be given more liquid. Thismethod can be used to achieve about a 20 degree temperature difference.One of the supplies could be lubricating oil or ozone while the othersupply could be a fuel having a high resistance to ignition, e.g. a highoctane number, to permit the SOC to be effectively controlled by varyingthe amount of oil or ozone added to the mixture. Also, by using theengine's lubricating oil supply, or using ozone created by the engineduring operation, an additional supply of fuel/additive can be avoided.

Equivalence Ratio

Another control variable that applicants have shown can be effectivelyused to control the SOC and combustion duration or heat release rate isthe equivalence ratio φ of the fuel/air mixture. Equivalence ratio isequal to fuel/air ratio divided by stoichiometric fuel/air ratio (if<1,fuel deficient; if>1, fuel excess). Combustion needs to be slowed downin a PCCI engine because fast combustion leads to high noise, loweredefficiency and high peak cylinder pressure. If different temperaturesand/or equivalence ratios can be achieved throughout the charge ofair/fuel at or near point of ignition, the resulting rate of combustionwill possibly be slowed down thus advantageously lengthening theduration of combustion. The equivalence ratio could be increased byincreasing the fuel flow to the cylinder without a correspondingincrease in intake air flow, or by decreasing the intake air flow. Theequivalence ratio could be lowered by decreasing the fuel flow to thecylinder without a corresponding decrease in air flow, or increasing theair flow rate. Variations in the quantity of fuel delivered to acylinder is varied by controlling the operation of fuel control valves39, 41, and/or fuel injectors 35, 36 in a known manner. The variationsin the air flow rate could be achieved by, for example, variablycontrolling compressor 24 to vary boost pressure.

To test the lower limit for equivalence ratio, applicants conductedengine studies to determine whether acceptable PCCI combustion could beobtained with an extremely lean mixture. The results indicate that verystable combustion can be achieved at an extremely lean equivalence ratioof 0.05 while obtaining a heat release duration of approximately 30degrees. Also, as shown in FIGS. 35 and 36, the results indicated thatthe start of combustion advances and the apparent heat release durationdecreases as equivalence ratio increases, i.e. air/fuel mixture becomesricher. Applicants have clearly shown, as indicated in FIG. 37, wherecylinder temperature increases indicate the heat release event.Moreover, referring to FIG. 38, the apparent heat release durationbecomes longer as equivalence ratio decreases, i.e. air/fuel mixturebecomes leaner. Also, applicant have shown that for a four stroke enginethat both peak cylinder pressure and GIMEP increase as equivalence ratiobecomes richer. With respect to a two-stroke engine, applicant havedetermined that as equivalence ratio increases, GIMEP increases.

Studies were also conducted to investigate whether the equivalence ratioaffects the amount of fuel burned in PCCI combustion. The resultsindicated that as equivalence ratio becomes richer, the percentage offuel energy showing up as apparent heat released increases at first andthen levels off near 80%. This number can never reach 100% because ofheat transfer. With respect to emissions, as equivalence ratio becomesricher, fuel specific hydrocarbon emissions decrease. In addition, asequivalence ratio became richer, average noise levels increased, andGIMEP increased. As equivalence ratio becomes richer, the average knockintensity increases. As equivalence ratio became richer, thecycle-to-cycle combustion variation, as measured by the coefficient ofvariation (COV) of GIMEP, generally decreased. In fact, the COV's ofGIMEP, for the conditions of the study, stayed below the combustionstability limit (in this case defined as 5%), where a COV above thelimit indicates unacceptable stability.

Studies were performed to determine the effect that variations inequivalence ratio have on thermal efficiency in PCCI combustion. Anequivalence ratio study was performed while matching the followingparameters: speed, IMT, IMP, engine oil temperature, and engine watertemperature. Equivalence ratio was increased by holding air flowconstant and increasing fuel flow to the engine. As fuel flow increasedand equivalence ratio became richer, gross indicated thermal efficiencyincreased at first and finally leveled off. Engine work output increasedwith respect to increased fuel flow as more fuel was burned. At theleaner equivalence ratios, a significant amount of fuel is leftunburned. At the richer equivalence ratios, the percentage of fuel thatis being burned levels off as noted hereinabove, and the gross indicatedthermal efficiency levels off because the increase in engine output isbeing offset by the additional fuel input.

In addition, an engine study was conducted with the engine cycle runningfrom bottom dead center of the compression stroke to BDC of theexpansion stroke. The study was conducted using a compression ratio of14.5:1, an engine speed of 1200 RPM, a BDC compression temperature of389 K, pressure at BDC of 4.31 bar, and no heat transfer. The fuel usedwas propane. The equivalence ratio was varied while all other parameterswere held constant. It was discovered that the percent of energyreleased slowly tapered off as the equivalence ratio drops below 0.15.This data indicates that for a given temperature and pressure, there isa lower limit to the equivalence ratio of a mixture that will burncompletely. Also, it was shown that FSCO emissions are very high atequivalence ratios below 0.15. This data indicates that only a smallamount of the fuel burns to completion at these low equivalence ratiosfor this temperature and pressure. In addition, the FSHC decreaseslightly as the equivalence ratio is varied from 0.05 to 0.4. Thus, mostof the fuel reacts regardless of the equivalence ratio. It was alsoshown that SOC occurs earlier as equivalence ratio increases. The studyshowed that peak cylinder temperature gradually increases as equivalenceratio is increased showing the increased amount of energy available tobe released. Peak cylinder pressure (PCP) gradually increases asequivalence ratio is increased showing the increased amount of energyavailable to be released. At equivalence ratios greater than or equal to0.18, virtually all of the available fuel energy is released, leading toa nearly linear increase in PCP as equivalence ratio increases.

Applicants have determined that it may be possible, although notnecessarily desirable, to maintain PCCI combustion at very richequivalence ratios, e.g. 0.5, if IMP and IMT are sufficiently low toprevent the peak cylinder pressure limit from being exceeded. It will bedifficult to start an engine at the low boost and IMT levels needed formaintaining low cylinder pressures at such rich equivalence ratios. Thevery advanced heat release, loud knock, and combustion roughness makerunning at this condition undesirable. A lower CR for retarding SOC mayimprove these aspects.

Also, by varying the level of charge stratification, the temperature andequivalence ratio distribution can be altered to permit control of thecombustion rate and/or the start of combustion. An auxiliary combustionchamber concept may be a mechanism for achieving the desiredstratification, thereby enabling better control over the start ofcombustion. For example, conventional auxiliary combustion chamberdesigns typically used on small engines having indirect injection (IDI),and large spark ignited engines using natural gas fuel, could be used.

In order to operate under the desired lean conditions for optimal PCCIcombustion, substantial air flow must be provided to the intakemanifold. A turbocharger could provide the needed air flow for amulti-cylinder PCCI engine. Applicants' original target was to reach anequivalence ratio of 0.40 or leaner. Referring to FIG. 39, applicantshave shown that operating at leaner than an equivalence ratio of 0.29would violate the compressor pressure ratio limit of the availableturbocharger. Applicant determined that turbine pressure ratios are veryhigh at lean equivalence ratios. As a result, the exhaust manifoldpressure is very high which causes a large BSFC penalty. Because of therelatively cool exhaust temperatures produced by PCCI combustion, verysmall turbine cases are needed which result in high exhaust manifoldpressures.

Applicants have determined that it would be desirable to operate underslightly leaner conditions than the original target. At an equivalenceratio less than 0.4, a smaller turbine casing was used to decrease thecompressor pressure ratio and exhaust manifold pressure ratio, but ahigh BSFC penalty is paid, as shown in FIG. 40. FIGS. 41 and 42illustrate the higher PMEP losses with the smaller turbine casing andthe higher BSFC. Also, with the smaller turbine casing, the rotor speedis much higher and, in fact, near the limit on rotor speed as seen inFIG. 43 (rotor speed limit 120-125 k rpm range). Applicants discoveredthat there is a lower limit on the size of the turbine casing used dueto the losses incurred with the high back pressure and with reaching therotor speed limit.

In order to avoid this problem with the high back pressure and rotorspeed limiting airflow, one possible solution is to use a mechanicallydriven supercharger in conjunction with a turbocharger. The superchargerwould be upstream of the compressor so that the turbine bears less of aburden for producing boost. Some BSFC penalty would be incurred for theshaft work absorbed by the supercharger; however, the BSFC penalty isless than the very high penalty incurred with the very small turbine.Because the supercharger is driven mechanically from the shaft, thereshould be no trouble getting the desired air flow. The turbine then canbe sized somewhat larger, and should not approach the speed limit andshould not have extremely high back pressure.

Applicants have also determined the effect of engine speed on SOC. Thetime of autoignition depends on the temperature and pressure histories.By changing the engine speed, these histories are changed. It ispossible to advance the combustion event by reducing the engine speed,and to retard the combustion event by increasing the engine speed.Specifically, a 75% increase in engine speed, from 1000 to 1750 resultedin a 1.5% increase in the start of combustion pressure and a 2.8%increase in the start of combustion temperature. In addition, a 75%increase in engine speed decreased the heat release rate duration by0.81 ms (only a 23% decrease) which corresponds to an increase in heatrelease duration of 1.7 crank angle degrees (only an 8% increase). Giventhis minimal impact of engine speed on the SOC and heat release, and theinability to effectively vary engine speed in many practical engineapplications, engine speed is not viewed as an effective combustioncontrol variable. However, one example where engine speed could be usedto provide some control over combustion is in an application where theengine drives a generator or alternator.

As discussed hereinabove, the foregoing control variables are used tocontrol the SOC and the duration of combustion to achieve optimum PCCIcombustion. One key consequence of efficient, optimum combustion isreduced emissions. Applicants have shown that a PCCI engine can achieveNOx emission levels that are well below any other NOx emission levelsever demonstrated by applicants using diesel and natural gas engines,and well below future emissions standards as shown in FIG. 44. The useof propane as the fuel resulted in the lowest NOx emissions relative todiesel fuel and gasoline.

Applicants have also determined the effect of the control variables andother factors on emissions of a PCCI engine. Engine speed has littleeffect on the quantity of NOx emissions. Although a 75% increase inengine speed approximately tripled the FSNOx, the levels of NOxemissions produced were still extremely low. Also, as equivalence ratiobecomes richer, fuel specific NOx generally increases, but still remainsat extremely low levels. Referring to FIG. 45, applicants havedetermined that engine speed appears to affect FSCO and FSHC emissionsmore significantly. As shown, below a certain critical speed, virtuallyall of the fuel burns, FSHC are low and FSCO is low. Just above thecritical speed, the fuel partially burns, resulting in higher FSCOemissions. As engine speed continues to increase, the percentage of thefuel that burns continues to drop, resulting in lower FSCO emissions.These emissions also vary as the temperature at BDC varies. Referring toFIG. 46, at very low temperatures, very little of the fuel burns,leading to high FSHC emissions. Since none of the fuel is burning atthese low temperatures, no carbon monoxide is produced. As thetemperature increases, a higher percentage of the fuel is burned, whichleads to increased production of carbon monoxide and lower FSHC.Finally, above a certain critical temperature, all of the fuel burnscompletely, leading to extremely low FSHC and FSCO emissions. In fact,as shown in FIG. 47, applicants have shown that all data points with endof combustion flame temperatures above 1600 K had acceptable COemissions. It has been shown that both high temperature and the hydroxylradical (OH) are critical for the desired oxidation of CO. Importantly,as equivalence ratio becomes richer, fuel specific CO decreases, whilethe concentration of CO₂ in the exhaust increases. In one study, allpoints taken with an equivalence ratio<0.2 had CO emissions above theEPA CO limit.

As equivalence ratio becomes richer, fuel specific HC decreases.Clearly, unburned hydrocarbons (UHC) are a key concern for PCCI enginessince reducing unburned hydrocarbons is essential to the commercialfeasibility of a PCCI engine. Applicants have determined that UHC, andCO, is formed in small crevices positioned in the components forming thecombustion chamber, i.e above the top ring of the piston between thepiston and the liner; between the cylinder head and the cylinder liner;and around the components mounted in the cylinder head. The crevicesprevent the volume of mixture in the crevice from reaching asufficiently high temperature necessary for burning of the HC andoxidation of the CO. For example, applicants have shown that similarpistons with different crevice volumes have different UHC levels. Thepresent PCCI engine may include one of several designs to minimize UHC.The present crevice minimizing designs result in a low crevice volume;keep the fuel away from any existing crevices; or cause the mixture inthe crevice volume to burn appropriately. The designs shown in FIGS. 48aand 48 b are most easily implemented in a ported two stroke cycleengine. Referring to FIG. 48a, in one embodiment, the engine has asingle piece head and liner combination 300, although a two-piece systemcould be used. Just above the top ring 302 (at TDC), the bore 304increases to eliminate the crevice around the top land 306 of piston308. There are no crevices in the cylinder head, as it is a single piecewithout valves, gaskets, etc.

Referring to FIG. 48b, a second embodiment of the crevice minimizingdesign may similarly include a one-piece head and liner 310. However, inthis embodiment, the piston 312 has a very aggressive cutback 314forming the top land to enlarge the crevice volume 316 between the topland and the liner. The crevice volume 316 is now so large that it willno longer quench combustion in this area thus allowing fuel in thisvolume to burn resulting in reduced UHC. FIG. 49 illustrates yet anotherembodiment including a cup or chamber 320 formed in the cylinder head322 of the engine. The fuel injector 324 is positioned to inject fueldirectly into cup 320 early in the compression stroke. Because air ispushed into cup 320, the fuel does not exit the cup. After compressionignition occurs, the products can pass through the relatively largepassage or throat 326 between the cup 320 and the main cylinder 328. Thefuel is well mixed because of the turbulence of the air entering thecup. Because there are no crevices in the cup and because the fuel doesnot leave the cup until after combustion is completed, UHC are extremelylow. The cup could easily be coated with a thermal barrier coating toreduce heat losses.

FIGS. 50a and 50 b illustrate a cup design for a four stroke engine. Theexhaust and intake valves 330 are arranged around a cup 332 in the head334. Cup 332 may be positioned directly above the combustion chamber 336as shown in FIG. 50a or offset to allow more room for the valves 330 asshown in FIG. 50b. Another possibility is to include a small auxiliaryvalve in the cup to allow the products to exit the cup more efficiently.This valve could open after the main exhaust valve opens so that theauxiliary exhaust valve in the cup would not open against a highpressure. In this case, the auxiliary exhaust valve could beelectronically operated. The timing of opening and closing of this valvecould be used to vary the residual mass fraction which would allowcontrol over the SOC using this auxiliary valve. Also, an opposed pistonengine, as discussed hereinabove, may be used to substantially reducethe crevice volume by avoiding a cylinder head and the associatedcrevices.

Now referring to FIG. 1a, another embodiment of the present inventionfor reducing emissions is disclosed. Specifically, this embodimentcontrols UHC and CO by heating the upper portion of the cylinder liner49 to cause oxidation of the charge in the crevices. A heater 51 isincorporated into the upper part of the liner. The heater could be anytype of heater capable of effectively producing heat, such as anelectrical resistance heater. The heater heats the gas in the creviceabove the top ring when the piston nears TDC. This heating will causethe gas to be less dense resulting in a smaller mass of charge remainingin the crevice. The charge leaving the crevice will be at a highertemperature due to the heating thus increasing the tendency of thecharge to react and form CO₂ instead of CO and UHC.

Also, a glow plug may be used to heat the combustion gases to reduceemissions by enabling a larger portion of the crevice volume to beburned. It has been determined by applicants that a glow plug will haveonly a slight impact on the SOC. Since SOC changes only slightly whenthe glow plug is turned on, it does not appear that the glow plug isinitiating combustion. It is more likely that when the glow plug, whichwas located in a spacer plate, is turned on, it gradually warms up thegas in the crevice volume. This increase in temperature is sufficient tospeed up the onset of rapid combustion, and burn more of the fuel thanwould have been burned without the glow plug on, resulting in a slightincrease in GIMEP.

The present engine, as shown in FIGS. 1a and 1 b, may also be operatedas a multi-mode engine which changes modes of operation based on theoperating conditions or needs of the particular application. Forinstance, the engine may be operated on diesel fuel only as aconventional diesel engine, as a modified diesel engine with diesel fuelbeing injected earlier in the compression event than the conventionaldiesel engine, as a spark-ignited engine using spark plug 56 (FIG. 1a)or as a PCCI engine. This type of spark ignited/compression ignited DI(direct injection) variable compression ratio engine provides acombination of low emissions, high power density, and ease of starting.

This engine operates in the following different modes depending on thecurrent operating conditions/needs of the engine.

1) Medium compression ratio (˜10:1), early injection (fuel injectedduring intake stroke or very early in the compression stroke) nearlyhomogeneous:

a) Overall lean mixture, spark ignited—allows low NOx, high brake meaneffective pressure (BMEP) operation, as well as medium BMEP operation.

b) Stoichiometric mixture, spark ignited—allows high NOx high BMEPtransient operation, as well as low NOx operation with a 3 way catalyst.

2) High compression ratio (˜15:1), early injection, nearly homogeneous,very lean (φ<0.5), compression ignition—allows very low NOx medium BMEPand low BMEP operation.

3) High compression ratio (˜15:1), late injection, stratified charge:

a) Spark ignited—allows medium NOx, medium BMEP unthrottled operation,and low BMEP operation.

b) Compression ignition—allows medium NOx medium and low BMEPunthrottled operation.

4) Low compression ratio (˜8:1), early injection, nearly homogeneous,spark ignited:

a) Lean burn—allows very high BMEP operation.

b) Stoichiometric—allows very high BMEP operation.

5) Medium compression ratio (˜10:1), late injection, stratified charge,spark ignited—allows medium NOx, medium and low BMEP, and high BMEPoperation.

6) Very high compression ratio (˜20:1), lean burn, early injection,nearly homogeneous, compression ignition—allows the engine to be startedin PCCI mode.

The key here is to take full advantage of the variable compressionratio. Starting of the engine can be achieved with spark ignition at alower compression ratio and then transitioning to high compressionratio, lean PCCI operation for low NOx. For less severe (e.g. not ascold) conditions, engine starting could be achieved directly with veryhigh compression ratio PCCI operation. At low and medium loads, theengine can operate in a PCCI mode as the compression ratio is adjustedto keep the start of combustion near the optimum crank angle. For highload requirements, the air/fuel ratio can be enriched, compression ratiolowered, and the engine can be spark ignited. In order to handle suddentransients, the engine may go into one of the late injection modes wherericher air/fuel ratios are possible without engine damage.

In the multi-mode engine, ECU 20 (FIG. 1) functions with a controlstrategy for controlling the various controlled features of the engineto effectively switch between, and operate in, the different modes inorder to achieve a variety of objectives. For example, the multi-modeengine achieves low NOx emissions in the PCCI mode while enhancingstartability by providing a high compression ratio or spark ignition. Inaddition, the engine can achieve a high cylinder pressure at high BMEPby switching to a lower compression ratio spark-ignited mode. Themulti-mode engine also permits stable combustion to occur afterswitching to late injection which results in a stratified charge byrapidly adjusting the compression ratio. Also, fuel consumption can beeffectively controlled using high compression, PCCI operation andstratified charge operation requiring no throttling which have excellentthermal efficiency. This operation also improves transient response bygoing from PCCI to late injection, stratified charge to suddenly enrichthe mixture. This multi-mode engine can also effectively minimize knock,and therefore knock damage, by effectively operating at lean PCCI orstratified charge or low compression ratio, lean burn or stoichiometricconditions. Of course, the engine operates to effectively control thestart of combustion during PCCI operation by varying, for example, asdiscussed hereinabove, the temperature and/or the equivalence ratioand/or the pressure and/or the air/fuel mixture autoignition properties.This engine could run on a variety of fuels like gasoline or dieselfuel.

Another operating mode is dual injection in which an early injection isused to create a lean charge for PCCI operation. A second, lateinjection then adds a small amount of stratified fuel which can beeither spark or compression ignited to help ignite the remaining fuel.This mode is similar to diesel pilot operation but would only be usedduring transition between the different modes of operation or duringengine starting. Applicants have studied the effects of diesel pilotoperation on emissions. FIG. 51 shows a comparison of the normalizedheat release rate versus crank angle for the three different dieselpilot injection quantities into a PCCI engine operating on propane. Amicro-pilot injection of 0.1% resulted in good heat release placementwith no measurable increase in FSNOx. A diesel pilot of an amountestimated to supply 3.6% of the fuel energy resulted in a heat releasecurve having substantially the same shape as the previous case. The SOCis slightly more advanced than that of the 0.1% case despite a lower IMTand constant equivalence ratio. Also, FSNOx emissions have increasedover the 0.1% case from zero to 3.9 g/kg. The final curves illustratesthe heat release for a case with ˜18% of the fuel energy coming from thediesel pilot. The heat release rate curve is shaped the same as theclassic diesel heat release rate curve with a premixed burn spike and adiffusion burn region. Also, the FSNOx (15.3 g/kg) and FSHC (478 g/kg)are significantly higher than in the cases with smaller diesel pilots.

With respect to diesel pilot injection, as the percentage of fuel energyfrom the pilot increases, the start of combustion (SOC) becomes moreadvanced, despite the lowering of IMT and a constant equivalence ratio.This earlier SOC is caused by the diesel fuel autoigniting earlier thanthe propane. As the percentage of pilot increases, the heat released bythe pilot during the compression stroke increases, leading to highertemperatures earlier in the cycle. Higher temperatures increase thechemical reaction rates of reactions involving propane, leading toearlier autoignition of the propane. Therefore, extremely low NOx levelsand good heat release placement can be achieved when using a very smalldiesel pilot or micropilot, preferably less than 4% of the total fuelenergy.

Applicants have also studied the control of noise associated with PCCIcombustion. Level of noise generated by PCCI combustion is related tothe knock intensity. Thus, as knock intensity is decreased, noisesdecreases. As shown in FIGS. 4a, 4 c and 6, lowering cylinder pressure,for example, by retarding the SOC, substantially decreases the knockintensity and, therefore, noise. The present engine and control systempermits continuous PCCI combustion with minimal noise by avoidingexcessive peak cylinder pressures while maintaining the requiredcylinder pressure necessary for efficient, low emission PCCI combustionand the desired power output.

The control system of the present invention operates to actively andvariably control the mixture's temperature, pressure, autoignitioncharacteristic and equivalence ratio to ensure that the combustion eventoccurs between 20 crank angle degrees BTDC and 35 crank angle degreesATDC. The control system achieves this function by using combustionsensor 16, e.g. pressure sensor, to signal the start of combustion orthe location of the heat release event for each cycle. Also, ECU 20,which receives the signals from sensor 16, determines whether the SOC isoccurring within a predetermined crank angle range and determineswhether the duration of combustion is within a predetermined desiredcrank angle range. One conventional way for the ECU to determine theoptimum SOC would be to use a look-up table. If the SOC and/or theduration of combustion are outside the predetermined crank angle range,then ECU 20 determines the appropriate control variable or variables toadjust, and generates and sends the appropriate signal 22 to the chosencontrol mechanism or mechanisms, e.g. air cooler 28, heater 30, glowplug 44, fuel control valves 39, 41, variable compression ratio device38, etc., as discussed hereinabove. The control variables are varied asrequired to maintain the timing of the start of PCCI combustionpreferably between 20 crank angle degrees BTDC and 10 crank angledegrees ATDC, and to maintain the duration of combustion in the range of5-30 crank angle degrees.

Applicants have determined that, in order to initiate and maintain PCCIcombustion upon start-up in a cold engine, the conditions in thecylinders, e.g. temperature and/or pressure, must be activelyinfluenced. For example, the intake air temperature could be raisedusing heater 30 and/or a glow plug 44, and/or the in-cylinder wallsheated using a cylinder wall heater 51 and/or an enginecoolant/lubricating oil heater. Also, the in-cylinder pressure andtemperature could be increased using variable compression ratio device38. Another effective control feature for enhancing startability is toadd small amounts of ozone to the intake air supply using injector 42,or into the cylinder using injector 40. Alternatively, or additionally,one of the fuel supplies could have a high autoignition property, e.g.low octane number. Also, the engine may be operated in a non-PCCI, forexample, as a spark-ignition, dual fuel or diesel engine, duringstarting of the engine. One or a combination of these controls arevaried, in accordance with the principles discussed hereinabove withrespect to each control feature, to cause PCCI combustion to occur. Asthe engine starts, the ECU will monitor the start of combustion andduration of combustion by receiving combustion data, e.g. pressuresignals, from sensor 16 throughout engine operation.

Once the engine is warmed up, the SOC and duration of combustion willvary due to the sensitivity of PCCI combustion to the temperature andpressure history. Small variations in the numerous factors affectingtemperature and pressure history, such as combustion chamber walltemperature, IMT, equivalence ratio, IMP, etc. result in significantvariation in the SOC and the duration of combustion. During operation,the control system of the present invention will vary one or more of thecontrol variables, that is, temperature, pressure, air/fuel mixtureautoignition properties and/or equivalence ratio, using the variouscontrol mechanisms discussed hereinabove, in such a manner to maintainthe SOC and duration of combustion in the desired ranges. For example,applicants have shown that SOC can be advanced from 5° ATDC to 0.5° BTDCby increasing the IMT from 184° F. to 195° F., as shown in FIG. 8.Applicants have also shown that increasing CR, which raises thein-cylinder temperatures, can be used to advance SOC. For example, FIG.21 shows that increasing CR from 14:1 to 22:1 advanced the SOC from 2°ATDC to 13° BTDC when the equivalence ratio was 0.35 and IMT was 380 K.In addition, applicants have shown that increasing RMF to raise thetemperature of the charge also can be used to advance SOC. When RMF wasincreased by adjusting exhaust valve lash from 0.025″ to 0.046″, the SOCadvanced from 6.4° ATDC to 1.7° ATDC, as shown in FIG. 16. Heat transferto the charge, whether from active heating elements or hot surfaces suchas the combustion chamber walls, has also been shown to advance SOC.Applicants have also shown that, with a glow plug installed in thecombustion chamber, the SOC retarded from 0.6° ATDC to 1.5° ATDC afterthe glow plug had been turned off, as shown in FIG. 11. Applicants havedetermined, as shown in FIG. 9, that increasing combustion chamber walltemperatures from 400 K to 933 K can advance the SOC from 7° ATDC to 14°BTDC.

With respect to pressure control, increasing IMP serves to advance theSOC. FIG. 31c, for example, shows that increasing IMP on the singlecylinder engine from 52 psia to 57 psia caused the SOC to advance from3.7° ATDC to 1.5° BTDC. Any method of affecting cylinder pressure, suchas varying compression ratio or changing valve timing, both illustratedabove, can be used to control SOC.

With respect to equivalence ratio, applicants have determined, as shownin FIG. 38, show that increasing equivalence ratio from 0.30 to 0.33 byincreasing fuel flow to the engine advanced the SOC from 5.5° ATDC to2.0° ATDC. Also, varying the autoignition properties of the air/fuelmixture by the addition of reactive species or even diluent can affectSOC. Applicants have shown that for the case shown in FIG. 33,increasing the amount of ozone added to the charge from 0 to 36 g/kg offuel had the effect of advancing SOC from 1° ATDC to 12.5° BTDC. In onestudy where diesel fuel was used in a pilot injection to initiate SOC inan air-propane mixture, the amount of pilot used affected SOC. Forexample, when pilot quantity was increased from approximately 0.1% to18% of the total fuel energy, the SOC advanced from 2° ATDC to 10° BTDC.In one study, EGR was used as a diluent to retard SOC while holding IMTconstant with an aftercooler. As shown in FIG. 17, when EGR rate wasincreased from 2.9% to 8.0%, the SOC retarded from 1.2° ATDC to 4.2°ATDC. Applicants have shown that increasing the air/fuel mixture'sresistance to autoignition by increasing octane number, for example, canbe used to retard SOC. Also, applicants have shown that when octanenumber was increased from 80 to 100, the SOC retarded from 14° BTDC to7° BTDC for a case where IMT plus reheat was 311 K.

Of course, any of these control variables could be adjusted in theopposite direction from the above examples to achieve the oppositeeffect on SOC if necessary. For example, rather than increasing IMT toadvance SOC, IMT could be decreased to retard SOC. Also, the magnitudesof such variations would be increased or decreased as necessary tomaintain the desired SOC.

Applicants have shown that the combustion or heat release duration canbe affected by varying different parameters. As SOC is retarded, theheat release duration increases. For example, FIG. 8 shows that as SOCis retarded, by reducing IMT from 195 degrees F. to 184 degrees F., theduration increases from approximately 6 degrees to approximately 24degrees. Similarly, increasing the equivalence ratio decreases the heatrelease duration. Applicants also believe that increasing the degree oftemperature and equivalence ratio stratification of the charge increasesthe heat release duration. However, given the difficulty of measuringthe degree of temperature or equivalence ratio stratification more workis needed to quantify the level of stratification.

Of course, given the relationship between SOC and duration, any controlstrategy that retards SOC should also increase the duration. Bymaintaining the SOC and the duration of combustion in the desired rangeswhile controlling the equivalence ratio to ensure lean burn conditions,the control system minimizes NOx emissions. Also, the present enginedesign, also reduces UHC and CO emissions by minimizing the crevices inthe cylinder thereby minimizing the unburned gases as shown in FIGS.48a-50 b.

During operation, balancing the combustion processes between thecylinders of the engine of FIG. 1b can be accomplished by varying any ofthe control variables used to control the SOC, as discussed hereinabove.The ECU 20 compares the SOC and duration of combustion data provided bysensor 16 for each cylinder. When the data indicates that the SOC and/orduration of combustion of one or more cylinders is occurring outside apredetermined crank angle range, the ECU will determine the appropriatecontrol variable or variables most effective for the given operatingconditions and generates a control signal for controlling the controlvariable to cause the SOC and/or duration of combustion to adjust so asto fall within the desired range. Applicants have determined thatcylinder balancing is best achieved by controlling equivalence ratio,adding ozone to the mixture, controlling individual heaters associatedwith each cylinder intake port, varying compression ratio using device38 or variable valve timing, adding oil via pilot injection or port fuelinjection, port injection of water and/or any of the methods discussedhereinabove for varying EGR or RMF. Any of these or other forms ofcombustion control could be used alone, or in a variety of combinations,to enhance combustion balancing control. For example, the combustioncontrol provided by the multiple fuel/additive system describedhereinabove could be enhanced by providing variable valve timing and/orcombustion chamber surface temperature cooling, e.g. engine coolant, orpiston cooling nozzle control. Also, one or more glow plugs 44 (FIG. 1a)may be used as an inexpensive, easy method of achieving at least partialcontrol over combustion balancing between the cylinders. It may also bepossible to control the EGR rate for each cylinder in order to balancecombustion quality.

Industrial Applicability

The present PCCI engine and control system may be used in any stationaryor nonstationary power plant, including any automotive, industrial,marine or military application. The present PCCI engine and controlsystem is especially advantageous in any power generation applicationwhere low emissions are desirable.

We claim:
 1. An internal combustion engine operable in a premixed chargecompression ignition mode, comprising: an engine body; a combustionchamber formed in the engine body for containing a mixture of fuel andair; combustion history control means for controlling a combustionhistory of future combustion events to optimize engine operation, saidcombustion history control means including at least one of a temperaturecontrol means for varying the temperature of the mixture of fuel andair, a pressure control means for ultimately varying the pressure of themixture, an equivalence ratio control means for varying an equivalenceratio of the mixture and a mixture autoignition property control meansfor varying an autoignition property of the mixture; engine operatingcondition detecting means for detecting an engine operating conditionindicative of the combustion history and generating an engine operatingcondition signal indicative of said engine operating condition; andprocessing means for receiving said engine operating condition signal,determining a combustion history value based on said engine operatingcondition signal, and generating one or more control signals based onsaid combustion history value, said one or more control signalscontrolling at least one of said temperature control means, saidpressure control means, said equivalence ratio control means and saidmixture autoignition property control means to variably control thecombustion history of future combustion events.
 2. The engine of claim1, wherein said processing means compares said combustion history valueto a predetermined desired combustion history value and generates saidone or more control signals based on the comparison of said combustionhistory value to said predetermined desired combustion history value,said at least one control signal controlling said at least one of saidtemperature control system, said pressure control system, saidequivalence ratio control system and said mixture autoignition propertycontrol system to cause said combustion history value to approach saidpredetermined desired combustion history value.
 3. The engine of claim1, wherein said engine operating condition detecting means includes astart of combustion sensor for sensing the start of combustion andgenerating a start of combustion signal, said combustion history valuebeing determined based on said start of combustion signal.
 4. The engineof claim 3, wherein said processing means compares said combustionhistory value to a predetermined desired combustion history value andgenerates said one or more control signals based on the comparison ofsaid combustion history value to said predetermined desired combustionhistory value, said at least one control signal controlling said atleast one of said temperature control system, said pressure controlsystem, said equivalence ratio control system and said mixtureautoignition property control system to cause said combustion historyvalue to approach said predetermined desired combustion history value.5. The engine of claim 3, wherein said start of combustion sensor is acylinder pressure sensor.
 6. The engine of claim 3, wherein saidcombustion history control means includes said temperature control meansand said pressure control means.
 7. The engine of claim 6, wherein saidpressure control means includes a compression ration varying means forvarying at least one of an effective compression ratio varying means forvarying at least one of an effective compression ratio and a geometriccompression ration so as to selectively vary the pressure in saidcombustion chamber to control a timing of the start of combustion. 8.The engine of claim 7, wherein said compression ration varying meansincludes a plunger movabley counted on said engine body adjacent saidcombustion chamber, said plunger movable from a retracted position intoan extended position toward said combustion chamber to decrease the sizeof said combustion chamber and increase the geometric compression ratio.9. The engine of claim 8, wherein said plunger is hydraulically actuatedinto the extended position.
 10. The engine of claim 7, wherein saidengine is an opposed piston engine.
 11. The engine of claim 10, whereinsaid opposed piston engine includes a first piston mounted on a firstcrankshaft and a second piston mounted on a second crankshaft oppositesaid first piston, said combustion chamber being formed between saidfirst and said second pistons, said compression ratio varying deviceincluding a phase shifting mechanism for varying a relative phase ofrotation between said first and said second crankshafts.
 12. The engineof claim 1, wherein said engine operating condition detecting means is acylinder pressure sensor.
 13. The engine of claim 1, wherein saidcombustion history control means includes said temperature control meansand said equivalence ratio control means.
 14. The engine of claim 1,wherein said combustion history control means includes said temperaturecontrol means and said mixture autoignition property control means. 15.The engine of claim 14, further including an intake air system fordelivering intake air to said combustion chamber, wherein said mixtureautoignition property control means includes a delivery device mountedon said engine body for delivery a reactive fluid into at least one ofsaid intake system and said combustion chamber to control at least oneof a timing of a start of combustion and a duration of combustion. 16.The engine of claim 15, wherein said delivery device delivers ozone toadvance the timing of the start of combustion.
 17. The engine of claim15, wherein said delivery device delivers ozone to advance the timing ofthe start of combustion.
 18. The engine of claim 14, further includingan intake air system for delivery intake air to said combustion chamberand an exhaust gas system for directing exhaust gas from said combustionchamber, wherein said mixture autoignition property control meansincludes an exhaust gas recirculation system for delivering exhaust gasfrom said exhaust gas system to said intake air system to dilute saidintake air so as to control a timing of a start of combustion.
 19. Theengine of claim 14, further including an intake air system for deliveryintake air to said combustion chamber and a fuel supply system connectedto said intake air system for directing fuel into one of said intake airsystem and said combustion chamber, said mixture autoignition propertycontrol means including a first fuel supply having a first autoignitionproperty and a second fuel supply having a second autoignition propertydifferent from said first auotignition property.
 20. The engine of claim1, wherein said combustion history control means includes said pressurecontrol means and said equivalence ratio control means.
 21. The engineof claim 1, wherein said combustion history control means includes saidpressure control means and said mixture autoignition property controlmeans.
 22. The engine of claim 1, wherein said combustion historycontrol means includes said equivalence ratio control means and saidmixture autoignition property control means.
 23. The engine of claim 1,further including an intake air system for delivering intake air to saidcombustion chamber, wherein said combustion history control meansincludes said temperature control means, said temperature control meansincluding at least one of an intake air temperature control means forcontrolling the temperature of the intake air or the mixture of air andfuel in the intake system and an in-cylinder temperature control meansfor controlling the temperature of the mixture in said combustionchamber.
 24. The engine of claim 23, wherein said temperature controlmeans includes said intake air temperature control means, said intakeair temperature control means including an air heater means positionedin said intake air system.
 25. The engine of claim 24, wherein theengine includes a plurality of combustion chambers, said intake airsystem including a respective intake port associated with each of saidplurality of combustion chambers for directing intake air to therespective combustion chamber, said air heater means including arespective intake air heater positioned in each respective intake duct.26. The engine of claim 23, wherein said intake air temperature controlmeans further includes an air cooler positioned in said intake airsystem.
 27. The engine of claim 23, further including an exhaust gassystem for directing exhaust gas from said combustion chamber, whereinsaid temperature control means includes said intake air temperaturecontrol means, said intake air temperature control means including anexhaust gas recirculation system for delivering exhaust gas from saidexhaust gas system to said intake air system to control intake airtemperature.
 28. The engine of claim 27, further including an aircompressor positioned in said intake air system for compressing theintake air, said exhaust gas recirculation system delivering exhaust tosaid intake air system upstream of said air compressor.
 29. The engineof claim 23, wherein said temperature control means includes said intakeair temperature control means, said intake air temperature control meansincluding a water injection device for injecting water into said intakeair system.
 30. The engine of claim 23, wherein the engine includes aplurality of combustion chambers, said intake air system including oneor more air manifolds for delivering intake air to said plurality ofcombustion chambers, further including a fuel supply system connected tosaid intake air system upstream of said one or more air manifolds fordirecting fuel into said intake air system.
 31. The engine of claim 30,wherein said fuel supply system includes a first fuel supply and asecond fuel supply, said first and said second fuel supplies havingdifferent autoignition properties.
 32. The engine of claim 23, whereinsaid temperature control means includes said in-cylinder temperaturecontrol means, said in-cylinder temperature control means including aresidual mass fraction control means for varying a residual massfraction of combustion products remaining in said combustion chamberfrom one combustion event to a subsequent combustion event.
 33. Theengine of claim 32, further including an exhaust port formed in saidengine body and an exhaust valve operable to open and close said exhaustport, wherein said residual mass fraction control means varies a timingof closing of said exhaust port by said exhaust valve to vary the amountof said residual mass fraction.
 34. The engine of claim 23, wherein saidengine body includes combustion chamber walls forming said combustionchamber, said temperature control means including said in-cylindertemperature control means, said in-cylinder temperature control meansincluding a combustion chamber wall temperature control means forvarying the temperature of said combustion chamber walls.
 35. The engineof claim 34, wherein said combustion chamber wall temperature controlmeans includes a coolant temperature control system for varying thetemperature of engine coolant to vary the temperature of said combustionchamber walls.
 36. The engine of claim 34, wherein said combustionchamber wall temperature control means includes an electric heatermounted on said engine body adjacent said combustion chamber walls. 37.The engine of claim 23, wherein said engine body includes an engineblock, a cylinder formed in said engine block and a cylinder head, saidtemperature control means includes said in-cylinder temperature controlmeans, said in-cylinder temperature control means including a glow plugmounted in said cylinder head for heating the mixture of air and fuel insaid combustion chamber.
 38. The engine of claim 23, further including arotatable crankshaft mounted on said engine body, a cylinder formed insaid engine body and a piston operatively connected to said crankshaftfor reciprocal movement in said cylinder, wherein said temperaturecontrol means includes said in-cylinder temperature control means, saidin-cylinder temperature control means including a compression ratiovarying means for varying at least one of an effective compression ratioand a geometric compression ratio of said cylinder.
 39. The engine ofclaim 38, wherein said compression ratio varying means includes aplunger movably mounted on said engine body adjacent said combustionchamber, said plunger movable from a retracted position into an extendedposition toward said combustion chamber to decrease the size of saidcombustion chamber and increase the geometric compression ratio of saidcylinder.
 40. The engine of claim 39, wherein said plunger ishydraulically actuated into the extended position.
 41. The engine ofclaim 38, wherein said engine is an opposed piston engine.
 42. Theengine of claim 41, wherein said opposed piston engine includes a firstpiston mounted on a first crankshaft and a second piston mounted on asecond crankshaft opposite said first piston, said combustion chamberbeing formed between said first and said second pistons, saidcompression ratio varying device including a phase shifting mechanismfor varying a relative phase of rotation between said first and saidsecond crankshafts.
 43. The engine of claim 38, further including anintake port formed in said engine body and an intake valve operable toopen and close said intake port, wherein said compression ratio varyingmeans varies the timing of closing of said intake port by said intakevalve to vary the effective compression ratio.
 44. The engine of claim23, wherein said temperature control means includes said in-cylindertemperature control means, said in-cylinder temperature control meansincluding an injector for injecting a fluid into said combustion chamberto vary the temperature of the mixture of air and fuel.
 45. The engineof claim 6, further including an intake air system for delivery intakeair to said combustion chamber, wherein said pressure control meansincludes an intake air pressure control means for varying the pressureof the intake air in said intake air system to vary the pressure of themixture in the combustion chamber.
 46. The engine of claim 45, whereinsaid intake air pressure control means includes a turbocharger mountedin said intake air system.
 47. The engine of claim 46, wherein saidintake air pressure control means further includes a bypass circuit forbypassing exhaust gas around said turbocharger and a waste gate valvepositioned in said bypass circuit for varying exhaust flow through saidbypass circuit.
 48. The engine of claim 45, wherein said intake airpressure control means includes a throttle valve positioned in saidintake air system.
 49. The engine of claim 1, further including anintake air system for delivering intake air to said combustion chamber,wherein said combustion history control means includes said mixtureautoignition property control means, said mixture autoignition propertycontrol means including a delivery device mounted on said engine bodyfor delivering a reactive fluid into at least one of said intake systemand said combustion chamber to control at least one of a timing of astart of combustion and a duration of combustion.
 50. The engine ofclaim 1, further including an intake air system for delivering intakeair to said combustion chamber and an exhaust gas system for directingexhaust gas from said combustion chamber, wherein said combustionhistory control means includes said mixture autoignition propertycontrol means, said mixture autoignition property control meansincluding an exhaust gas recirculation system for delivering exhaust gasfrom said exhaust gas system to said intake air system to dilute saidintake air so as to control a timing of a start of combustion.
 51. Theengine of claim 1, further including an intake air system for deliveringintake air to said combustion chamber and a fuel supply system connectedto said intake air system for directing fuel into one of said intake airsystem and said combustion chamber, wherein said combustion historycontrol means includes said mixture autoignition property control means,said mixture autoignition property control means including a first fuelsupply having a first autoignition property and a second fuel supplyhaving a second autoignition property different from said first autoignition property.
 52. The engine of claim 1, further including acombustion chamber crevice minimizing means for minimizing the formationof unburned hydrocarbons in combustion chamber crevices duringcombustion.
 53. The engine of claim 52, wherein said engine bodyincludes a cylinder block including a cylinder and a cylinder head,further including a piston reciprocally mounted in said cylinder to formsaid combustion chamber, said crevice minimizing means including acutback formed in said piston adjacent said combustion chamber forenlarging a crevice volume.
 54. The engine of claim 52, wherein saidengine body includes a cylinder block including a cylinder and acylinder head, said crevice volume minimizing means including acombustion cup formed in said cylinder head in communication with saidcombustion chamber.
 55. The engine of claim 52, wherein said engine bodyincludes a cylinder block including a cylinder and a cylinder head,further including a piston reciprocally mounted in said cylinder to formsaid combustion chamber, said crevice minimizing means including aheater means positioned adjacent said combustion chamber for heating themixture in the crevices.
 56. The engine of claim 1, further including arotatable crankshaft and a piston operatively connected to saidcrankshaft for reciprocal movement through a top dead center position,wherein said one or more control signals controls at least one of saidtemperature control means, said pressure control means, said equivalenceratio control means and said mixture autoignition property control meansto variably control the combustion history of future combustion eventsto cause the start of combustion to occur between 20 crank angle degreesbefore said top dead center position and 10 crank angle degrees aftersaid top dead center position.
 57. The engine of claim 56, wherein saidone or more control signals controls at least one of said temperaturecontrol means, said pressure control means, said equivalence ratiocontrol means and said mixture autoignition property control means tovariably control the combustion history of future combustion events tocause combustion to occur over a range of 5-30 crank angle degrees. 58.The engine of claim 1, further including a plurality of combustionchambers, at least one of said plurality of combustion chambersoperating in a premixed charge compression ignition mode and theremaining combustion chambers operating in a diesel mode.
 59. The engineof claim 58, further including an exhaust gas recirculation systemconnected to said at least one cylinder operating in a premixed chargecompression ignition mode.
 60. The engine of claim 1, wherein saidengine body includes an engine block and a plurality of cylinders formedin said engine block, each of said plurality of cylinders including acombustion chamber, said temperature control means including a cylindertemperature compensating means for heating the mixture of air and fuelin at least two of said combustion chambers to compensate for heat loss.61. The engine of claim 60, further including an engine coolant systemformed in said engine body for circulating engine coolant, wherein saidcylinder temperature compensating means includes an engine coolantcontrol system for controlling at least one of a coolant temperature anda coolant flow rate of the coolant in said coolant system.
 62. Theengine of claim 1, wherein said engine includes a plurality ofcombustion chambers formed in the engine body, an intake air system forsupplying intake air to said plurality of combustion chambers, and anexhaust system for directing exhaust gas from said plurality ofcombustion chambers, said combustion history control means controlling acombustion history of future combustion events in each of said pluralityof combustion chambers to optimize engine operation, further including acombustion balancing means for variably adjusting operating conditionsin each of said plurality of combustion chambers to achieve a similarcombustion history for combustion events of said plurality of combustionchambers to balance combustion between said plurality of combustionchambers.
 63. The engine of claim 62, wherein said exhaust systemincludes a respective exhaust port associated with each of saidplurality of combustion chambers and formed in said engine body, and arespective exhaust valve operable to open and close said exhaust port atpredetermined times during operation of the engine, wherein saidcombustion balancing means includes a variable exhaust valve timingcontrol means associated with each of said plurality of combustionchambers for receiving a variable valve timing control signal from saidprocessor and varying the timing of closing of said exhaust port by saidrespective exhaust valve to vary an amount of residual exhaust gasremaining in said combustion chamber after a combustion event so as tobalance combustion events between said plurality of combustion chambers.64. The engine of claim 62, wherein said intake system includes arespective intake port associated with each of said plurality ofcombustion chambers and formed in said engine body, and a respectiveintake valve operable to open and close said respective intake port atpredetermined times during operation of the engine, wherein saidcombustion balancing means includes a variable intake valve timingcontrol means associated with each of said plurality of combustionchambers for receiving a variable valve timing control signal from saidprocessor and varying the timing of closing of said respective intakeport by said respective intake valve so as to balance combustion eventsbetween said plurality of combustion chambers.
 65. The engine of claim62, wherein said combustion balancing means includes an injector mountedon said engine body for injecting a balancing fluid into one of saidintake system and said plurality of combustion chambers, said balancingfluid chancing t he autoignition property of the mixture.
 66. The engineof claim 65, wherein said balancing fluid is at least one of a fuel,water, oil, oxygen and ozone.
 67. The engine of claim 62, wherein saidintake system includes a respective intake port associated with each ofsaid plurality of combustion chambers and form ed in said engine body,said combustion balancing means including a respective heater mounted ineach of said respective intake ports for receiving heater signals forvariably controlling the temperature of the intake air.
 68. The engineof claim 62, wherein said combustion balancing means includes a variablecompression ratio means associated with each of said plurality ofcombustion chambers for varying a compress ion ratio of each of saidplurality of combustion chambers to maintain combustion balance betweensaid plurality of combustion chambers.
 69. The engine of claim 62,wherein said combustion balancing means includes a fuel supply systemconnected to said intake air system for directing fuel into said intakeair system, wherein said fuel supply system includes a first fuel supplyand a second fuel supply, said first and said second fuel supplieshaving different autoignition properties.
 70. The engine of claim 62,wherein said engine body includes combustion chamber walls forming eachof said plurality of combustion chambers, said combustion balancingmeans including a combustion chamber wall temperature control means forvarying the temperature of said combustion chamber walls.
 71. The engineof claim 70, further including an engine coolant system formed in saidengine body for circulating engine coolant, wherein said combustionchamber wall temperature control means includes a coolant temperaturecontrol system for varying the temperature of engine coolant in saidengine coolant system to vary the temperature of said combustion chamberwalls.
 72. The engine of claim 70, wherein said combustion chamber walltemperature control means includes an electric heater mounted on saidengine body adjacent said combustion chamber for heating said combustionchamber walls.
 73. The engine of claim 62, wherein said combustionbalancing means includes a glow plug mounted on said engine bodyadjacent said combustion chamber for heating the mixture of air and fuelin said combustion chamber.
 74. The engine of claim 62, wherein saidcombustion balancing means includes an equivalence ratio varying meansassociated with each of said plurality of combustion chambers forvarying an equivalence ratio in each of said plurality of combustionchambers to maintain combustion balance between said plurality ofcombustion chambers.
 75. The engine of claim 62, wherein said combustionbalancing means includes a combustion chamber temperature control meansassociated with each of said plurality of combustion chambers forcontrolling the temperature of the mixture in each combustion chamber,said combustion chamber temperature control means including a residualmass fraction control means for varying a residual mass fraction ofcombustion products remaining in each combustion chamber from onecombustion event to a subsequent combustion event to maintain combustionbalance between said plurality of combustion chambers.
 76. A premixedcharge compression ignition internal combustion engine, comprising: anengine body; a plurality of cylinders formed in the engine body; arespective piston mounted in each of said plurality of cylinders forreciprocal movement, each respective piston defining a combustionchamber for containing a mixture of fuel and air; an intake air systemfor supplying intake air to said plurality of cylinders; an exhaustsystem for directing exhaust gas from said plurality of cylinders;combustion history control system for controlling a combustion historyof future combustion events in said combustion chamber of each of saidplurality of cylinders to optimize engine operation, said combustionhistory control system including to optimize engine operation, saidcombustion history control system including at least two of atemperature control system for ultimately varying the temperature of themixture of fuel and air, a pressure control system for ultimatelyvarying the pressure of the mixture, and equivalence ration controlsystem for varying an equivalence ratio of the mixture and a mixtureautoignition property control system for varying an autoignitionproperty of the mixture; engine operating condition detecting device fordetecting an engine operating condition indicative of the combustionhistory and generating an engine operating condition signal indicativeof said engine operating condition; and a processor for receiving saidengine operating condition signal, determining a combustion historyvalue based on said engine operating condition signal, and generatingone or more control signals based on said combustion history value, saidone or more control signals controlling at least one of said temperaturecontrol system, said pressure control system, said equivalence ratiocontrol system and said mixture autoignition property control system tovariably control the combustion history of future combustion events. 77.The engine of claim 76, wherein said engine operating conditiondetecting means including a respective combustion sensor mounted in eachof said plurality of cylinders for sensing at least one of a start ofcombustion and a duration of combustion and generating a combustionsignal, said combustion history value being determined for eachcombustion based on said combustion signal.
 78. The engine of claim 77,further including a cylinder combustion balancing means for variablyadjusting operating conditions in said combustion chamber of each ofsaid plurality of cylinders to achieve a similar combustion history forcombustion events of said plurality of cylinders to balance combustionbetween said plurality of cylinders.
 79. The engine of claim 78, whereinsaid exhaust system includes a respective exhaust port associated witheach of said plurality of cylinders and formed in said engine body, andand exhaust value operable to open and close said exhaust port atpredetermined times during operation of the engine, wherein saidcylinder combustion balancing means includes a variable exhaust valvetiming control means associated with each of said plurality of cylindersfor receiving a variable valve timing control signal from said processorand varying the timing of closing of said exhaust port by saidrespective exhaust valve to vary an amount of residual exhaust gasremaining in said combustion chamber after a combustion event so as tobalance combustion events between said plurality of cylinders.
 80. Theengine of claim 78, wherein said intake system includes a respectiveintake port associated with each of said plurality of cylinders andformed in said engine body, and a respective intake valve operable toopen and close said respective intake port at predetermined times duringoperation of the engine, wherein said cylinder combustion balancingmeans includes a variable intake valve timing control valve timingcontrol signal from said processor and varying the timing of closing ofsaid respective intake port by said respective intake valve so as tobalance combustion events between said plurality of cylinders.
 81. Theengine of claim 78, wherein said cylinder combustion balancing meansincludes an injector mounted on said engine body for injecting abalancing fluid into one of said intake system and said combustionchamber, said balancing fluid changing the autoignition property of themixture.
 82. The engine of claim 81, wherein said balancing fluid is atleast one of a fuel, water, oil, oxygen and ozone.
 83. The engine ofclaim 78, wherein said intake system includes a respective intake portassociated with each of said plurality of cylinders and formed in saidengine body, said cylinder combustion balancing means including arespective heater mounted in each of said respective intake ports forreceiving heater signals for variably controlling the temperature of theintake air.
 84. The engine of claim 78, wherein said cylinder combustionbalancing means includes a variable compression ratio means associatedwith each of said plurality of cylinders for varying a compression ratioof each of said plurality of cylinders to maintain combustion balancebetween said plurality of cylinders.
 85. The engine of claim 78, whereinsaid cylinder combustion balancing means includes a fuel supply systemconnected to said intake air system for directing fuel into said intakeair system, wherein said fuel supply system includes a first fuel supplyand a second fuel supply, said first and said second fuel supplieshaving different autoignition properties.
 86. The engine of claim 78,wherein said cylinder combustion balancing means includes a glow plugmounted on said engine body adjacent said combustion chamber for heatingthe mixture of air and fuel in said combustion chamber.
 87. The engineof claim 78, wherein said cylinder combustion balancing means includesan equivalence ratio varying means associated with each of saidplurality of cylinders for varying an equivalence ratio in each of saidplurality of cylinders to maintain combustion balance between saidplurality of cylinders.
 88. The engine of claim 78, wherein saidcylinder combustion balancing means includes an in-cylinder temperaturecontrol means associated with each of said plurality of cylinders forcontrolling the temperature of the mixture in each combustion chamber,said in-cylinder temperature control means including a residual massfraction control means for varying a residual mass fraction ofcombustion products remaining in each combustion chamber from onecombustion event to a subsequent combustion event to maintain combustionbalance between said plurality of cylinders.
 89. The engine of claim 77,wherein said engine body includes combustion chamber walls forming saidcombustion chamber, said cylinder combustion balancing means including acombustion chamber wall temperature control means for varying thetemperature of said combustion chamber walls.
 90. The engine of claim89, further including an engine coolant system formed is said enginebody for circulating engine coolant, wherein said combustion chamberwall temperature control means includes a coolant temperature controlsystem for varying the temperature of engine coolant is said enginecoolant system to vary the temperature of said combustion chamber walls.91. The engine of claim 89, wherein said combustion chamber walltemperature control means includes an electric heater mounted on saidengine body adjacent said combustion chamber for heating said combustionchamber walls.
 92. The engine of claim 77, wherein said combustionhistory control system includes said temperature control system, saidtemperature control system including at least one of an intake airtemperature control means for controlling the temperature of the intakeair or the mixture of air and fuel in the intake system and anin-cylinder temperature control means for controlling the temperature ofthe mixture in the combustion chamber.
 93. The engine of claim 92,wherein said temperature control system includes said intake airtemperature control means, said intake air temperature control meansincluding at least one of an air heater positioned in said intake airsystem and an air cooler positioned in said intake air system.
 94. Theengine of claim 92, wherein said temperature control system includessaid intake air temperature control means, said intake air temperaturecontrol means including an exhaust gas recirculation system fordelivering exhaust gas from said exhaust gas system to said intake airsystem to control intake air temperature.
 95. The engine of claim 92,wherein said temperature control system includes said intake airtemperature control means, said intake air temperature control meansincluding a water injection device for injecting water into said intakeair system.
 96. The engine of claim 92, wherein said temperature controlsystem includes said in-cylinder temperature control means, saidin-cylinder temperature control means including a residual mass fractioncontrol means for varying a residual mass fraction of combustionproducts remaining in said combustion chamber from one combustion eventto a subsequent combustion event.
 97. The engine of claim 96, furtherincluding an exhaust port formed in said engine body and an exhaustvalve operable to open and close said exhaust port in timed relation toa combustion event, wherein said residual mass fraction control meansvaries the timing of closing of said exhaust port by said exhaust valveto vary the amount of said residual mass fraction.
 98. The engine ofclaim 92, wherein said engine body includes combustion chamber wallsforming said combustion chamber, said temperature control systemincluding said in-cylinder temperature control means, said in-cylindertemperature control means including a combustion chamber walltemperature control means for varying the temperature of said combustionchamber walls, said combustion chamber wall temperature control meansincluding at least one of a coolant temperature control system forvarying the temperature of an engine coolant to vary the temperature ofsaid combustion chamber walls and an electric heater mounted on saidengine body adjacent said combustion chamber for heating said combustionchamber walls.
 99. The engine of claim 92, wherein said temperaturecontrol system includes said in-cylinder temperature control means, saidin-cylinder temperature control means including a glow plug mounted onsaid engine body for heating the mixture of air and fuel in saidcombustion chamber.
 100. The engine of claim 92, wherein saidtemperature control system includes said in-cylinder temperature controlmeans, said in-cylinder temperature control means including an injectorfor injecting a fluid into said combustion chamber to vary thetemperature of the mixture of air and fuel.
 101. The engine of claim 77,wherein said pressure control system includes a compression ratiovarying means for varying at least one of an effective compression ratioand a geometric compression ratio so as to selectively vary the pressurein said combustion chamber to control a timing of the start ofcombustion.
 102. The engine of claim 101, wherein said compression ratiovarying means includes a plunger movably mounted on said engine bodyadjacent said combustion chamber, said plunger movable from a retractedposition into an extended position toward said combustion chamber todecrease the size of said combustion chamber and increase the geometriccompression ratio.
 103. The engine of claim 101, wherein the engine isan opposed piston engine including a first piston mounted on a firstcrankshaft and a second piston mounted on a second crankshaft oppositesaid first piston, said combustion chamber being formed between saidfirst and said second pistons, said compression ratio varying deviceincluding a phase shifting mechanism for varying a relative phase ofrotation between said first and said second crankshafts.
 104. The engineof claim 77, wherein said pressure control system includes an intake airpressure control means for varying the pressure of the intake air insaid intake air system to vary the pressure of the mixture in saidcombustion chamber.
 105. The engine of claim 104, wherein said intakeair pressure control means includes a turbocharger mounted in saidintake air system.
 106. The engine of claim 77, wherein said mixtureautoignition property control system includes a delivery device mountedon said engine body for delivering a reactive fluid into at least one ofsaid intake system and said combustion chamber to control at least oneof a timing of the start of combustion and a duration of combustion.107. The engine of claim 77, further including a fuel supply systemconnected to said intake air system for directing fuel into said intakeair system, said mixture autoignition property control system includinga first fuel supply having a first autoignition property and a secondfuel supply having a second autoignition property different from saidfirst autoignition property.
 108. The engine of claim 77, furtherincluding a combustion chamber crevice minimizing means for minimizingthe formation of unburned hydrocarbons in combustion chamber crevicesduring combustion.
 109. The engine of claim 108, wherein said creviceminimizing means includes a cutback formed in said piston adjacent saidcombustion chamber for enlarging a crevice volume.
 110. The engine ofclaim 108, wherein said engine body includes a cylinder block and acylinder head, said crevice volume minimizing means including acombustion cup formed in said cylinder head in communication with saidcombustion chamber.
 111. The engine of claim 108, wherein said enginebody includes a cylinder block and a cylinder head, said crevice volumeminimizing means including a heater positioned adjacent said combustionchamber for heating the mixture positioned in combustion chambercrevices.
 112. The engine of claim 77, further including a rotatablecrank shaft mounted on said engine body, said piston being operativelyconnected to said crankshaft for reciprocal movement through a top deadcenter position, wherein said one or more control signals controls atleast one of said temperature control system, said pressure controlsystem, said equivalence ratio control system and said mixtureautoignition property control system to variably control the combustionhistory of future combustion events to cause the start of combustion tooccur between 20 crank angle degrees before said top dead center and 10crank angle degrees after said top dead center position.
 113. The engineof claim 112, wherein said one or more control signals controls at leastone of said temperature control system, said pressure control system,said equivalence ratio control system and said mixture autoignitionproperty control system to variably control the combustion history offuture combustion events to cause combustion to occur over a range of5-30 crank angle degrees.
 114. The engine of claim 77, wherein at leastone of said plurality of cylinders operates in a premixed chargecompression ignition mode and the remaining cylinders operate in adiesel mode.
 115. The engine of claim 114, further including an exhaustgas recirculation system for receiving exhaust gas flow from said atleast one cylinder operating in a premixed charge compression ignitionmode and directing the exhaust gas into intake air flowing into saidremaining cylinders operating in a diesel mode.
 116. A multi-modeinternal combustion engine capable of operating in a plurality of modesfor initiating combustion, comprising: an engine body; a combustionchamber formed in the engine body; an intake air system for deliveryintake air to said combustion chamber; at least one of a fuel injectionmeans mounted on said engine body for injecting fuel into one of saidcombustion chamber and said intake system while the engine operates in adiesel mode and a spark-ignition means mounted on said engine body forproviding a spark for initiating combustion in said combustion chamberwhile the engine operates in a spark-ignition mode; a premixed chargecompression ignition mode control means for operating the engine in apremixed charge compression mode, said premixed charge compressionignition mode control means including combustion history control meansfor controlling a combustion history of future combustion events tooptimize engine operation, said combustion history control meansincluding at least one of a temperature control means for ultimatelyvarying the temperature of the mixture of fuel and air, a pressurecontrol means for ultimately varying the pressure of the mixture, anequivalence ratio control means for varying an equivalence ratio of themixture and a mixture autoignition property control means for varying anautoignition property of the mixture, said premixed charge compressionignition mode control means including an engine operating conditiondetecting means for detecting an engine operating condition indicativeof the combustion history and generating an engine operating conditionsignal indicative of said engine operating condition, and a premixedcharge compression ignition processing means for receiving said engineoperating condition signal, determining a combustion history value basedon said engine operating condition signal, and generating one or morecontrol signals based on said combustion history value, said one or morecontrol signals controlling at least one of said temperature controlmeans, said pressure control means, said equivalence ratio control meansand said mixture autoignition property control means to variably controlthe combustion history of future combustion events; and a modeprocessing means for transferring engine operation between said premixedcharge compression ignition mode and at least one of said diesel andsaid spark-ignition modes.
 117. The engine of claim 116, furtherincluding a cylinder formed in said engine body, a rotatable crankshaftmounted on the engine body and a piston operatively connected to saidcrankshaft for reciprocal movement, said pressure control meansincluding a variable compression ratio means for varying one of aneffective compression ratio and a geometric compression ratio of saidcylinder between a first compression ratio and a second compressionratio, said mode processing means causing said cylinder to operate insaid spark-ignited mode when said cylinder is operated at said firstcompression ratio and transferring operation of said cylinder to saidpremixed charge compression ignition mode when said cylinder isoperating at said second compression ratio.
 118. The engine of claim116, wherein said engine operating condition detecting means includes astart of combustion sensor for sensing the start of combustion andgenerating a start of combustion signal, said combustion history valuebeing determined based on said start of combustion signal.
 119. Theengine of claim 118, wherein said premixed charge compression ignitionprocessing means compares said combustion history value to apredetermined desired combustion history value and generates said atleast one control signal based on the comparison of said combustionhistory value to said desired combustion history value.
 120. A premixedcharge compression ignition internal combustion engine, comprising: anengine body; a plurality of cylinders formed in the engine body; arespective piston mounted in each of said plurality of cylinders forreciprocal movement, each respective piston defining a combustionchamber for containing a mixture of fuel and air; an intake air systemfor supplying intake air to said plurality of cylinders; an exhaustsystem for directing exhaust gas from said plurality of cylinders;combustion history control system for controlling a combustion historyof future combustion events in said combustion chamber of each of saidplurality of cylinders to optimize engine operation, said combustionhistory control system including at least one of a temperature controlsystem for ultimately varying the temperature of the mixture of fuel andair, a pressure control system for ultimately varying the pressure ofthe mixture, an equivalence ratio control system for varying anequivalence ratio of the mixture and a mixture autoignition propertycontrol system for varying an autoignition property of the mixture;engine operating condition detecting device for detecting an engineoperating condition indicative of the combustion history and generatingan engine operating condition signal indicative of said engine operatingcondition; a processor for receiving said engine operating conditionsignal, determining a combustion history value based on said engineoperating condition signal, and generating one or more control signalsbased on said combustion history value, said one or more control signalscontrolling at least one of said temperature control system, saidpressure control system, said equivalence ratio control system and saidmixture autoignition property control system to variably control thecombustion history of future combustion events; and a cylindercombustion balancing means for variably adjusting operating conditionsin said combustion chamber of each of said plurality of cylinders toachieve a similar combustion history for combustion events of saidplurality of cylinders to balance combustion between said plurality ofcylinders.
 121. The engine of claim 120, wherein said exhaust systemincludes a respective exhaust port associated with each of saidplurality of cylinders and formed in said engine body, and an exhaustvalve operable to open and close said exhaust port at predeterminedtimes during operation of the engine, wherein said cylinder combustionbalancing means includes a variable exhaust valve timing control meansassociated with each of said plurality of cylinders for receiving avariable valve timing control signal from said processor and varying thetiming of closing of said exhaust port by said respective exhaust valveto vary an amount of residual exhaust gas remaining in said combustionchamber after a combustion event so as to balance combustion eventsbetween said plurality of cylinders.
 122. The engine of claim 120,wherein said intake system includes a respective intake port associatedwith each of said plurality of cylinders and formed in said engine body,and a respective intake valve operable to open and close said respectiveintake port at predetermined times during operation of the engine,wherein said cylinder combustion balancing means includes a variableintake valve timing control means associated with each of said pluralityof cylinders for receiving a variable valve timing control signal fromsaid processor and varying the timing of closing of said respectiveintake port by said respective intake valve so as to balance combustionevents between said plurality of cylinders.
 123. The engine of claim120, wherein said cylinder combustion balancing means includes aninjector mounted on said engine body for injecting a balancing fluidinto one of said intake system and said combustion chamber, saidbalancing fluid changing the autoignition property of the mixture. 124.The engine of claim 123, wherein said balancing fluid is at least one ofa fuel, water, oil, oxygen and ozone.
 125. The engine of claim 120,wherein said intake system includes a respective intake port associatedwith each of said plurality of cylinders and formed in said engine body,said cylinder combustion balancing means including a respective heatermounted in each of said respective intake ports for receiving heatersignals for variably controlling the temperature of the intake air. 126.The engine of claim 120, wherein said cylinder combustion balancingmeans includes a variable compression ratio means associated with eachof said plurality of cylinders for varying a compression ratio of eachof said plurality of cylinders to maintain combustion balance betweensaid plurality of cylinders.
 127. The engine of claim 120, wherein saidcylinder combustion balancing means includes a fuel supply systemconnected to said intake air system for directing fuel into said intakeair system, wherein said fuel supply system includes a first fuel supplyand a second fuel supply, said first and said second fuel supplieshaving different autoignition properties.
 128. The engine of claim 120,wherein said engine body includes combustion chamber walls forming saidcombustion chamber, said cylinder combustion balancing means including acombustion chamber wall temperature control means for varying thetemperature of said combustion chamber walls.
 129. The engine of claim128, further including an engine coolant system formed in said enginebody for circulating engine coolant, wherein said combustion chamberwall temperature control means includes a coolant temperature controlsystem for varying the temperature of engine coolant in said enginecoolant system to vary the temperature of said combustion chamber walls.130. The engine of claim 128, wherein said combustion chamber walltemperature control means includes an electric heater mounted on saidengine body adjacent said combustion chamber for heating said combustionchamber walls.
 131. The engine of claim 120, wherein said cylindercombustion balancing means includes a glow plug mounted on said enginebody adjacent said combustion chamber for heating the mixture of air andfuel in said combustion chamber.
 132. The engine of claim 120, whereinsaid cylinder combustion balancing means includes an equivalence ratiovarying means associated with each of said plurality of cylinders forvarying an equivalence ratio in each of said plurality of cylinders tomaintain combustion balance between said plurality of cylinders. 133.The engine of claim 120, wherein said cylinder combustion balancingmeans includes an in-cylinder temperature control means associated witheach of said plurality of cylinders for controlling the temperature ofthe mixture in each combustion chamber, said in-cylinder temperaturecontrol means including a residual mass fraction control means forvarying a residual mass fraction of combustion products remaining ineach combustion chamber from one combustion event to a subsequentcombustion event to maintain combustion balance between said pluralityof cylinders.
 134. A method for controlling a combustion history offuture combustion events in a combustion chamber of an internalcombustion engine operable in a premixed charge compression ignitionmode, comprising: detecting an engine operating condition indicative ofthe combustion history; generating an engine operating condition signalindicative of said engine operating condition; processing said engineoperating condition signal and determining an actual combustion historyvalue based on said engine operating condition signal; generating atleast one control signal based on said actual combustion history value;providing a combustion history control system for controlling acombustion history of future combustion events in the combustion chamberto optimize engine operation, said combustion history control systemincluding at least one of a temperature control system for ultimatelyvarying the temperature of a mixture of fuel and air for combustion inthe combustion chamber, a pressure control system for ultimately varyingthe pressure of the mixture, an equivalence ratio control system forvarying an equivalence ratio of the mixture and a mixture autoignitionproperty control system for varying an autoignition property of themixture; and providing said at least one control signal to at least oneof said temperature control system, said pressure control system, saidequivalence ratio control system and said mixture autoignition propertycontrol system to variably control the combustion history of futurecombustion events to optimize engine operation.
 135. The method of claim134, further including the steps of comparing said actual combustionhistory value to a predetermined desired combustion history value andgenerating said at least one control signal based on the comparison ofsaid actual combustion history value to said desired combustion historyvalue, said at least one control signal controlling said at least one ofsaid temperature control system, said pressure control system, saidequivalence ratio control system and said mixture autoignition propertycontrol system to cause said actual combustion history value to approachsaid predetermined desired combustion history value.
 136. The method ofclaim 134, further including a start of combustion sensor for sensingthe start of combustion and generating a start of combustion signal,said actual combustion history value being determined based on saidstart of combustion signal.
 137. The method of claim 136, furtherincluding the step of controlling said temperature control system tocause the start of combustion to occur earlier by increasing thetemperature of the mixture.
 138. The method of claim 137, furtherincluding the steps of providing a rotatable crankshaft and a pistonoperatively connected to said crankshaft for reciprocal movement througha top dead center position and controlling said temperature controlsystem to cause the start of combustion to occur between 20 crank angledegrees before said top dead center position and 10 crank angle degreesafter said top dead center position by varying the temperature of themixture.
 139. The method of claim 136, further including the step ofcontrolling said pressure control system to cause the start ofcombustion to occur earlier by increasing the pressure of the mixture.140. The method of claim 139, further including the steps of providing arotatable crankshaft and a piston operatively connected to saidcrankshaft for reciprocal movement through a top dead center positionand controlling said pressure control system to vary the pressure of themixture to cause the start of combustion to occur between 20 crank angledegrees before said top dead center position and 10 crank angle degreesafter said top dead center position.
 141. The method of claim 136,further including the step of controlling said equivalence ratio controlsystem to cause the start of combustion to occur earlier by increasingthe equivalence ratio of the mixture.
 142. The method of claim 141,further including the steps of providing a rotatable crankshaft and apiston operatively connected to said crankshaft for reciprocal movementthrough a top dead center position and controlling said equivalenceratio control system to vary the equivalence ratio of the mixture tocause the start of combustion to occur between 20 crank angle degreesbefore said top dead center position and 10 crank angle degrees aftersaid top dead center position.
 143. The method of claim 136, furtherincluding the step of controlling said mixture autoignition propertycontrol system to increase the autoignition property of the mixture inthe combustion chamber to cause the start of combustion to occurearlier.
 144. The method of claim 143, further including the steps ofproviding a rotatable crankshaft and a piston operatively connected tosaid crankshaft for reciprocal movement through a top dead centerposition and controlling said mixture autoignition property controlsystem to vary the autoignition property of the mixture in thecombustion chamber to cause the start of combustion to occur between 20crank angle degrees before said top dead center position and 10 crankangle degrees after said top dead center position.
 145. The method ofclaim 136, further including the step of controlling said equivalenceratio control system to decrease the equivalence ratio of the mixture tocause a duration of combustion to increase.
 146. The method of claim145, further including the steps of providing a rotatable crankshaft anda piston operatively connected to said crankshaft for reciprocalmovement, and controlling said equivalence ratio control system to varythe equivalence ratio of the mixture to cause a duration of combustionto occur over a range of 5-30 crank angle degrees.
 147. The method ofclaim 134, further including the steps of providing an engine bodycontaining a plurality of combustion chambers, and variably adjustingoperating conditions in one or more of said plurality of combustionchambers to cause said actual combustion history value associated witheach of said plurality of combustion chambers to approach a desiredcombustion history value for balancing combustion between said pluralityof combustion chambers.
 148. The method of claim 147, further includingthe step of providing a fuel supply system for directing fuel into airfor combustion in said plurality of combustion chambers and controllingsaid equivalence ratio control system to vary the quantity of fueldelivered to one or more of said plurality of combustion chambers tocause said actual combustion value associated with each of saidplurality of combustion chambers to approach a desired combustionhistory value for balancing combustion between said plurality ofcombustion chambers.
 149. The method of claim 147, further including anintake air system for supplying intake air to said plurality ofcombustion chambers, wherein the step of variably adjusting operatingconditions includes a step of supplying a balancing fluid into one ofsaid intake system and at least one of said plurality of combustionchambers to change the autoignition property of the mixture for said atleast one of said plurality of combustion chambers to balance combustionbetween said plurality of combustion chambers.
 150. The method of claim149, wherein said balancing fluid includes ozone.
 151. The method ofclaim 147, wherein said temperature control system includes a respectiveheater associated with each of said plurality of combustion chambers,wherein the step of variably adjusting operating conditions includes thestep of controlling said heaters to vary the temperature of the mixturein the combustion chamber to balance combustion between said pluralityof combustion chambers.
 152. The method of claim 151, further includingan intake air system for supplying intake air to said plurality ofcombustion chambers, said intake air system including a respectiveintake port associated with each of said plurality of combustionchambers, each of said heaters being positioned along a respectiveintake port for heating one of the mixture and a supply of intake air.153. The method of claim 147, wherein said pressure control systemincludes a respective variable compression ratio control systemassociated with each of said plurality of combustion chambers, said stepof variably adjusting operating conditions including variablycontrolling a compression ratio of each combustion chamber for balancingcombustion between said plurality of combustion chambers.
 154. Themethod of claim 147, wherein said temperature control system includes arespective glow plug associated with each of said plurality ofcombustion chambers, said step of variably adjusting operatingconditions including variably controlling said respective glow plug tovary the temperature of the mixture in the respective combustion chamberfor balancing combustion between said plurality of combustion chambers.155. The method of claim 147, further including an engine body, anexhaust port formed in said engine body and an exhaust valve means forcontrolling the flow through said exhaust port in timed relation to acombustion event, wherein said temperature control system includes aresidual mass fraction control means for varying a residual massfraction of combustion products remaining in at least one of saidplurality of combustion chambers from one combustion event to asubsequent combustion event, said step of variably adjusting operatingconditions including controlling said residual mass fraction controlmeans to vary the flow through said exhaust port by operating saidexhaust valve means to vary the amount of said residual mass fraction ina respective combustion chamber to balance combustion events betweensaid plurality of combustion chambers.
 156. The method of claim 155,wherein said exhaust valve means includes an exhaust valve operable toopen and close said exhaust port in timed relation to a combustionevent, said step of variably adjusting operating conditions includingcontrolling said residual mass fraction control means to vary the timingof closing of said exhaust port by said exhaust valve to vary the amountof said residual mass fraction in a respective combustion chamber tobalance combustion events between said plurality of combustion chambers.